Minimize Artemis-I

Artemis I — formerly Orion / EM-1 (Exploration Mission-1)

Orion Vehicle   ESM    Development Status    Launch    Payloads    References 

In March 2018, NASA renamed the former Orion / EM-1 (Exploration Mission-1) to Artemis I. Artemis I will be the first integrated test of NASA’s deep space exploration systems: the Orion spacecraft, Space Launch System (SLS) rocket and the ground systems at Kennedy Space Center in Cape Canaveral, Florida. The first in a series of increasingly complex missions, Artemis I will be an uncrewed flight test that will provide a foundation for human deep space exploration, and demonstrate our commitment and capability to extend human existence to the Moon and beyond. 1)

Orion EM-1, previously known as SLS-1 (Space Launch System-1) is NASA's first planned flight of the Space Launch System and the second uncrewed test flight of the Orion MPCV (Multi-Purpose Crew Vehicle). NASA, ESA, European and US Industry have teamed to develop the ORION spacecraft.

Under an agreement between NASA and ESA, ratified in December 2012, NASA’s new Orion vehicle for human space exploration missions includes the ESM (European Service Module), based upon the design and experience of ESA’s ATV (Automated Transfer Vehicle), the supply craft for the ISS (International Space Station).

ESA’s industrial prime contractor for ATV, Airbus Defence and Space of Bremen, Germany, is leading a European industrial consortium, developing this vehicle on behalf of ESA and working closely with NASA’s Orion US industrial prime contractor Lockheed Martin Space Systems.

Orion is the spacecraft that NASA intends to use to send humans and cargo into space beyond low earth orbit and to return them safely to Earth. It is being developed for crewed missions to cislunar space, asteroids, and then to Mars. The capsule is also planned as a backup vehicle for missions to the ISS (International Space Station). It will be launched by the NASA-developed SLS (Space Launch System) in 2019. 2) 3)

The first test flight of Orion was successfully completed in December 2014 with a Delta IV launch vehicle that launched the Orion Crew Module into a high elliptical orbit to demonstrate high-speed atmospheric Earth re-entry. This flight test did not include the ESM.

It is planned such that the Orion EM-1 flies a mission profile similar to what might be used in a future asteroid redirect mission. The un-crewed Orion travels to a lunar DRO (Distant Retrograde Orbit) mission (Figure 2), then returns on a trajectory calculated to achieve a high speed atmospheric entry on the order of ~11 km/s to demonstrate the performance and effectiveness of the Orion TPS (Thermal Protection System), as well as relevant environments prior to the first manned launch of the system. The total mission duration is 25 days (6 at destination). This will be the first flight of the ESM.

The human exploration of space is a national policy of the government of the United States. The National Space Policy directs NASA to: 4)

• Set far reaching exploration milestones. By 2025, begin crewed missions beyond the moon, including sending humans to an asteroid. By the mid-2030s, send humans to orbit Mars and return them safely to Earth.

• Furthermore, the NASA Authorization Act of 2010, a law passed by the U.S. Congress and signed by the President, states that the “long term objective for human exploration of space should be the eventual international exploration of Mars.”

NASA is implementing this policy as the Journey to Mars, a journey that will be neither quick nor easy. 56 million kilometers away at its closest approach, with an atmosphere too thin for easy braking but too thick to ignore, with freezing surface temperatures, a minimal magnetic field for radiation protection, and communications delays with Earth of up to 40 minutes, Mars represents the current high frontier in human exploration.

Even though Mars is tremendously challenging, it has resources necessary for human exploration (oxygen, CO2 atmosphere, and water). These resources are critical to allow us to break the ties with Earth and become Earth Independent. The atmosphere, even though very thin by Earth standards, still provides some radiation shielding. Developing the ability to utilize the resources on Mars will be critical for the journey. We have calculated that roughly 20 mt of oxygen will be needed for the human Mars ascent vehicle to achieve orbit around Mars. Rather than carry all of the propellant and oxygen needed for a Mars ascent vehicle, we will generate that propellant from the materials available on Mars.

The challenges are too difficult to tackle all at once. Instead, NASA is breaking it down into more manageable objectives: the Earth Reliant phase, the Proving Ground phase, and the Earth Independent phase. Each phase builds upon the successes (and failures) of the previous one in a sustainable, repeatable, and in manner that allows for changes in technology or funding. In this approach NASA does not need to develop and control all aspects of the journey. NASA will utilize the private sector and international partners in critical roles of the journey and depend on these partners for successful achievement of the overall journey.

Earth Reliant: NASA is operating in the Earth Reliant phase of the Journey to Mars aboard the ISS (International Space Station) right now. The ISS, orbiting some 400 km above Earth, is mere hours away from the safety and comfort of our home planet. Aboard the space station, NASA and the other international partners are developing the technologies needed to sustain human life much farther away than 400 kilometers. A new and varied fleet of commercially produced and procured vehicles is taking over the duties of transportation of humans and cargo from Earth to ISS. NASA’s investments in this area promise to create new opportunities for the development of LEO, including broader use of the ISS as an orbital science laboratory and as a demonstration platform for future commercial space facilities as NASA moves towards the Proving Ground phase.

In the Earth Reliant phase, NASA is developing the “Mars-capable” systems that will be needed for long-duration stays outside of the comfortable frontier of LEO. Currently manifested or planned experiments and demonstrations include improved long-duration life support for Mars missions, advanced fire safety equipment, next-generation spacesuit technologies, high-data-rate communications, techniques to reduce logistics, large deployable solar arrays, in-space additive manufacturing, advanced exercise and medical equipment, radiation monitoring and shielding, human/robotic operations, and autonomous crew operations.

However, these “Mars-capable” systems are not only technological, but also biological- this work includes the development and demonstration of the human systems; the countermeasures, procedures, and adaptations the crew will need to survive and thrive in deep space. NASA’s Human Research Program is actively working on identifying, mitigating, and eliminating the risks of spaceflight to the human body aboard ISS, while acknowledging that some risks- like radiation- can only be fully quantified with long-duration human exposure to the environment outside the Van Allen belt. NASA astronauts and others will also gain experience on a variety of management, operations, and maintenance styles and techniques are they begin flying to orbit onboard the Boeing and SpaceX crew vehicles.

We have a lot to learn from the Earth Reliant time on ISS. We have continuously been surprised by problems that arise on ISS, especially in the life support systems. NASA performed extensive ground testing on these systems only to be surprised by their actual performance in space. For example, the water systems were much more susceptible to bio-films and blockage than ground tests showed. Carbon dioxide removal system beds have more problems with dust generation and valve fouling than anticipated. We need to discover and solve these problems on ISS before venturing into deep space with these systems. ISS is the perfect platform for these development and testing activities.

In this Earth Reliant phase- when regular interaction and management from the ground is possible - NASA and its commercial partners will continue to return benefits to humanity on Earth while developing the skills to go farther. NASA intends to begin short-duration cislunar while ISS is still operating. It is a fundamental tenant of human spaceflight that continuity of operations be persevered, in order to maintain our progress in a sustained manner.

Earth Independence will also require a new operating philosophy with our crews. Today, the ground crews often serve as an additional ISS crew member. Many robotic activities are done from the ground while the ISS crew sleeps. During space walks the ground serves as an extra set of eyes and ears for the crew. As crews move into deep space, the crews must become more autonomous. Here again, ISS is an excellent platform to practice crew independence before it is required. Time delays between Earth and ISS can be added to simulate the real time delays associated with communication distances as will be experienced at Mars distances.

Proving Ground: Aboard NASA’s Orion spacecraft, astronauts will look down on Earth from a perspective never seen before. Far from the comparative hustle and bustle of the ISS- with the Earth speeding by the window, with 12-15 vehicle dockings per year, and with hundreds of government and commercial experiments running in constant communication with the ground- the Proving Ground will be a more secluded place. Beginning with missions of short duration and gradually building as experience is gained, the Proving Ground will allow NASA and its partners to practice with, innovate on, and demonstrate the technologies and capabilities needed to send humans to Mars, while remaining in a location near enough to Earth to allow for crew return (in a matter of days) and close monitoring of technology advancement. NASA recently issued a call for commercial industry to propose habitation concepts and solutions for the Proving Ground, continuing the partnership started in LEO.

Activities that have become what passes for routine in our industry- such as vehicle rendezvous and docking and EVA- will needed to be revalidated in cislunar space. The environmental, power, communications, and other systems that have been developed on ISS will be verified in the environment for which they were actually designed, far from regular resupply, and operating without the regularity of maintenance which they currently require.

Launching from the Kennedy Space Center in 2019, the first integrated flight of the SLS (Space Launch System) rocket and the Orion spacecraft, called EM-1 (Exploration Mission-1), will demonstrate NASA’s commitment and capability to extend human existence to deep space. The EM-1 mission will be flown without a crew. EM-1 is designed to stress the propulsion, navigation, communication, thermal, and Earth reentry systems. The mission will be the first mission flown to a distant retrograde orbit around the Moon, which is unique in that objects in this orbit will remain there without propulsive maneuvers. Testing the systems before the crew is flown is an important technique to reduce risks with the first crew missions to this remote location. The life support carbon dioxide removal system for Orion is being operated on ISS today.

The EM-1 milestone achievement will strengthen confidence in SLS and Orion as the right system design for the Journey to Mars strategy. The systems on Orion, and future deep space habitation systems, are designed to be Mars-class systems. EM-1 and subsequent missions will take these systems from Mars-class to “Mars Ready.” After a series of these missions, each increasing in duration and complexity, NASA will undertake a “shakedown cruise”- a long-duration mission using the “Mars-capable” systems, uninterrupted by outside assistance. This mission will validate the complete architecture needed to take humans to the Mars vicinity and return them to the Earth.

Earth Independent: Earth Independent systems and operations are NASA’s ultimate goal for Mars or any destination for humans beyond the Earth-Moon system. While true Earth Independence is many years away, NASA is laying the foundations for human exploration now. A fleet of robotic orbiters, landers, and rovers is on and around Mars, doing increasingly sophisticated analysis and exploration. Many of these missions have experiments explicitly dedicated to categorizing the environment humans will face; the Curiosity rover has a radiation detector that was also flown on ISS, and the upcoming Mars 2020 mission will have several more human health-related experiments. Robotic exploration is human exploration, albeit from a slightly removed distance, and both programs are tightly coordinated today. A safe human exploration of Mars cannot happen without a robust robotic foundation.

While the Earth Reliant and Proving Ground phases have been vigorously pursued and evaluated, the Earth Independent phase is less detailed. This is no accident. It will take an over a decade to get humans to Mars in a sustainable manner, and it is incumbent upon the current generation not to dictate or limit the manner that future generations will explore. While we can predict may of the needs of future explorers- radiation protection, food supply, environmental control, and so on- it is foolish to believe that our proposed technological solutions will be the ones most relevant to them. Instead, NASA is pursuing a capabilities-based approach, developing what we need as we can foresee the application. It is through this long-term view that we believe we can best serve our goal and destination of expanding the human presence in the solar system. We are developing an agile and sustainable approach to deep space exploration. Just as Apollo required a different approach to system engineering and hardware development, so too will the challenges associated with Mars-class missions require a different development approach and a new type of systems engineering. NASA and the U.S. alone cannot build all of the systems and perform all of the development needed for this adventure. NASA can orchestrate the plan, but will be dependent on the private sector and international partners for key components.

Today NASA is utilizing the ambitions of SpaceX to land a vehicle on Mars to obtain critical data on the technical considerations for using a propulsive landing capability in the Mars atmosphere. NASA is assisting SpaceX by providing deep space navigation capability and communication capability in exchange for access to SpaceX’s data on retro-propulsion Martian entry descent and landing data. NASA has also placed the European Space Agency in the critical path for all of its human deep space exploration capability by partnering with ESA to provide the Orion service module. The service module provides thermal control, power generation life support consumables storage and propulsion for Orion, allowing it to return to Earth from a distant retrograde orbit around the Moon. These functions are critical to keeping the crew safe on Orion.

A Marketplace Above: As NASA prepares to move beyond low Earth orbit, it is our goal to facilitate an orderly, timely, and profitable transition from government tenancy in LEO to the commercial sector. Through NASA’s commercial development programs, we have already demonstrated the ability of the private sector to deploy reliable launch and return vehicles for cargo to the ISS. In the near future, we are aiming to repeat that feat by using the world’s first commercially developed crew vehicles for ISS transportation. Earlier this year, with NASA’s assistance, the first commercially-developed expandable module was deployed onboard ISS.

Learning the benefits and issues with expandable modules directly in flight will provide criticality data for future planning. Rather than speculating on the properties of this new technology, direct on-orbit performance will be recorded. In ISS’s normal mode of operations, we see dozens of commercial payloads operating every day, from biological research to materials development to CubeSat deployment. The Center for the Advancement of Science (CASIS), NASA’s chosen operator for the U.S. National Laboratory portion of the ISS, is actively developing new markets and new opportunities for companies and even industries that have never previously considered spaceborne research. The goal is to expose the private sector directly to unique properties of space for their terrestrial based processes and let them see if there is a potential revenue generating opportunity in spaceborne research and manufacturing. These private sector companies can utilize to explore and test revenue generating concepts without a major investment in infrastructure. Transportation for both cargo and crew is already available from the private sector.

At the moment, the ISS is the only system in LEO. NASA and its international partners- Canada, Japan, and Russia- have committed to operating the ISS through at least 2024 (European confirmation of support is expected later this year). NASA does not intend to continue owning and operating a LEO platform. Through the research and development onboard ISS, we are trying to help create a new marketplace for both supply and demand in LEO- one where companies that require access to LEO for research or even production contract directly with companies that can provide transportation and logistics, without government involvement. We expect many of the approaches pioneered for commercial utilization of LEO will also have applications in NASA’s deep space activities. Commercialization of LEO (Low Earth Orbit) is the next frontier for private companies for both those that want to provide access and accommodations in space, and those that require the same.

The commercial LEO environment will likely be very different than ISS. It is unlikely that a facility as large and complex as the ISS will be built in LEO by the private sector. The facilities for the private sector are likely to be single purpose laboratories. The facilities could be crew tended and primarily ground operated. The facilities could also be extensions of current cargo vehicles or crew vehicles such as Cygnus, Dragon Lab or Dreamchaser. The facilities need to have low operating costs and reflect the revenue generation potential of the space research. The goal is a rich LEO research and manufacturing environment supported by a private sector transportation infrastructure.

Conclusion: It is a modern cliché to say that every generation believes they are living in a special time, with choices to be made that will positively or negatively affect the very future of humanity. It is true that the promise of Mars exploration and space commercialization has been made and broken- before, and it is tempting to believe that this time will be no different. However, we are at a point in space travel that is demonstrably unprecedented in human history. Privately developed and operated vehicles are delivering cargo to an international outpost that has been continually crewed for 15+ years, onboard which a commercial module is undergoing testing, and NASA has asked for concepts for the private sector to use the ISS to accelerate their development of revenue generation from space.

Private companies can now develop their own rockets and propulsion systems and sell them on the open market. Inside the ISS, experiments in nearly every scientific field are being conducted by commercial, industrial, and academic organizations, some of which are even looking to space as a production environment. We are also flying numerous pieces of terrestrial research equipment such as DNA sequencers. The private sector no longer needs to develop custom equipment but can fly their off-the-shelf research equipment to space. In the near future, commercial companies will begin ferrying astronauts to and from the ISS. And in public, in forums such as this, NASA is explicitly saying that not only is a commercial marketplace its desired and primary outcome for LEO, it is saying that a robust commercial space market is a fundamental building block for deep space human exploration.

Things are changing. As the Earth Reliant phase exits governmental control, NASA will take both its international and commercial partners to the Proving Ground, where we will learn to live and work farther from Earth than ever before in a sustainable manner. There is no set path for this journey to Mars- merely a set of frontiers that must be broken. There is no final frontier only the next one in front of us. We are beginning an exciting journey to move human presence off of the Earth and into the solar system.

Table 1: The NASA Exploration Program – the Journey to Mars 4) 5) 6)

Orion EM-2 is planned as a Crewed High Lunar Orbit mission no later than the end of 2021. It is planned to spend several days in lunar orbit before performing a TEI (Trans-Earth Injection) burn to begin the return to Earth. The total mission duration is expected to be 14 days maximum (4 at destination).




EM-1 - Lunar (DRO (Distant Retrograde Orbit) mission

- Qualification (uncrewed)
- Simulate asteroid redirect mission

25 days (6 at destination)

EM-2 - Crewed High Lunar Orbit mission

- Qualification (crewed)

14 days (4 at destination)

Lunar Sortie mission

- Land crew of four on the surface of the Moon
and returns them to Earth

26 days (7 uncrewed in LLO)

ISS Backup Crew Delivery mission

- Backup crew and cargo delivery to the ISS

216 days (210 quiescent)

Table 2: Overview of Orion ESM Design Reference Missions


Figure 1: Artist's rendition of the Orion EM-1 spacecraft in lunar orbit (image credit: NASA, ESA)


Figure 2: Orion EM-1 (Exploration Mission-1) design reference (image credit: NASA)

The Orion Vehicle

The Orion architecture configuration consists of the following modules: (Figures 3 and 4, Ref. 2)

• CM (Crew Module)

• ESM (European Service Module)

• CMA (Crew Module Adapter)

• SA (Spacecraft Adapter)

• SAJ (Spacecraft Adapter Jettisoned Fairings)

• LAS (Launch Abort System)

The Service Module (SM) refers to the combined CMA + ESM + SA + SAJ.

The Crew Module and ESM (European Service Module), also referred to as SM, are physically interfacing via an interface ring called the CMA (Crew Module Adapter). The ESM is attached to the CMA for the duration of the mission. Just prior to the Earth’s orbit entry, the CMA separates from the CM for CMA/ESM disposal and the CM performs final reentry and landing operations.

NASA is responsible for development of the CM, CMA, SA, SAJ, and LAS elements of the Orion spacecraft. The CMA provides the structural, mechanical, electrical, and fluid interface between the CM and ESM. In addition, the CMA houses communication equipment, sublimators for thermal heat rejection, and power and data control/interface electronics. The SM is enclosed by three spacecraft adapter fairing panels (SAJ) which provide a partial load path from the CMA to SA but also protect the solar arrays, radiators, and thrusters from launch and ascent loads. The fairings will be jettisoned during the ascent phase or following main engine cut-off of the launch vehicle.

The SA (Spacecraft Adapter) provides the interface to the launch vehicle during launch. During launch and ascent, the ESM and SA will be enclosed by the SAJ. The SA attaches to the aft end of the ESM to the Launch Vehicle and includes the structural interface, separation mechanisms, and umbilical connectors for communication between the launch vehicle and the Orion Spacecraft. At launch vehicle burnout, the Orion Spacecraft separates from the SA at the ESM/SA separation plane.


Figure 3: Overview of the Orion spacecraft architecture (image credit: NASA, ESA)


Figure 4: Orion schematic layout (image credit: NASA)

Orion EM-1 CM (Crew Module)

The milestones for the Orion EM-1 mirror the path taken by the Orion EFT-1 (Exploration Flight Test-1) spacecraft. However, the Orion EM-1 will sport a number of improvements based on the experiences of the December 2014 test flight. NASA is beefing up the critical TPS (Thermal Protection System) that will protect astronauts from the searing heats experienced during reentry as the human rated vehicle plunges through the Earth’s atmosphere after returning from ambitious expeditions to the Moon and beyond.

Based in part on lessons learned from EFT-1, engineers are refining Orion’s heat shield to enhance the design, ease manufacturing procedures and significantly strengthen is heat resistant capabilities for the far more challenging space environments and missions that lie ahead later this decade and planned further out in the future as part of NASA’s agency-wide ‘Journey to Mars’ initiative to send humans to the Red Planet in the 2030s.

On all future flights starting with EM-1 (Exploration Mission-1), the Orion crew module must withstand the higher temperatures and speeds experienced during return from more distant destinations such as the Moon, near-Earth Asteroids and Mars. Orion's TPS is comprised of the 5 m diameter main heat shield covering the rounded base of the capsule as well as the grid of back shell tiles bonded around the vehicle from top to bottom. 7)

Starting with EM-1, engineers will bond Orion’s thermal protection system back shell tiles with a silver, metallic-based thermal control coating. The coating is designed to keep Orion’s back shell in a temperature range from approximately -65 to 290ºC prior to entry and afford protection against electrical surface charges in space and during reentry.

The pressure vessel is the primary structure of Orion’s crew module and is made of seven large aluminum pieces that must be welded together in detailed fashion. The first weld connected the tunnel to the forward bulkhead, which is at the top of the spacecraft and houses many of Orion’s critical systems, such as the parachutes that deploy during reentry. Orion’s tunnel, with a docking hatch, will allow crews to move between the crew module and other spacecraft. 8)

Orion’s pressure vessel is composed of seven large pieces of aluminum, three of which are the cone panels. The pressure vessel holds the atmosphere astronauts will breathe against the vacuum of deep space, forming the crew compartment. The three panels together form the angled mid-section around the crew module where the windows and hatch are located. While technicians have been joining other elements of the structure together since early September, the cone panels have presented a unique challenge for NASA and Lockheed Martin, the agency’s prime contractor for Orion. Engineers who have sought to reduce the crew module’s overall weight have encountered and overcome technical challenges. 9)

The lessons learned from the EFT-1 mission are being applied to the EM-1 (Exploration Mission-1) and EM-2 flight test configurations to optimize a system design that can smoothly transition into production.

Ten of the most important lessons from EFT-1 focused on the ability to evaluate the design with actual flight performance. This was critical for the remaining design process as NASA continues to develop the most advanced Human rated spacecraft ever built. The following are the top ten lessons learned from this test flight: 10)

1) Some deep space designs are classic for a reason: Every aspect of Orion’s design is driven by crew safety. Over 50 years of NASA’s investment learning the ins and outs of human spaceflight has provided direction for meeting deep space requirements. An example is LAS (Launch Abort System). About 6 minutes into launch, the LAS is jettisoned to save mass for the journey to deep space destinations. While other system configurations exist, design trade studies repeatedly highlighted the advantage of not carrying extra weight past the time it is needed. So because the Orion LAS supports missions to deep space, mass is king and any extra weight is an extreme hindrance to those missions. By shedding the Orion LAS early, this mass isn’t a burden to the vehicle for the entire mission, and other Orion systems are able to provide the abort function for the remainder of ascent to orbit.

2) Crew safety is built in, not bolted on: The EFT-1 tested and verified systems that are built “into the bones” of the spacecraft from the very beginning. This means not just the heat shield or the flight computers are designed for the rigors of deep space, but everything included in the fundamental systems and structure of the spacecraft are designed and built to specifications set forth by NASA. Every system design has a deep space requirement it is being built to right now: Orion’s seats are being designed to help prevent loss of consciousness as astronauts experience up to 5 G’s during high-velocity re-entries, the cooling system keeps the crew cabin about 25ºC despite its heat shield being heated to 2,200ºC during reentry, the built in stowage lockers are designed to double as a safe-haven during dangerous solar activity, the life support system allows for exercise since deep space missions require much longer stays in zero gravity, computers and avionics are designed to self-correct in case there is a failure and you’re months from home, and the crew module tiles are designed to protect from multiple micro-meteoroid strikes since the number of strikes will increase during missions that last months instead of days.

3) Reusability must be tied to reality: Part of flying for the first time in space is being able to make informed decisions about what we can realistically reuse following a deep space mission. After evaluating areas of water intrusion and corrosion, we’ve come to expect that many components in the crew module, especially inside the pressurized volume, or the hull where the crew sits, can be reused for later flights—components such as the computers, avionics and electrical distribution for example. The structure itself is more difficult to predict for reuse base on the unpredictable landing loads it might experience from a long journey from deep space with unpredictable landing sea conditions. The program is looking at options for reuse based on actual landing load data provided.

4) Designs mature as we Learn: Significant design changes are being made to optimize the EM vehicles. Thefuture design and analysis efforts will be simplified (Figure 5), overall mass has gone down, and recurring costs for production will be lowered. Establishing a common design philosophy has prevented a large number of engineering revisions and hardware changes. The Orion design is now incorporating lessons from EFT-1 and updated requirements for the crewed EM-2 mission.


Figure 5: Some highlights of the numerous design changes made as a result of the EFT-1 flight (image credit: NASA, Lockheed Martin)

5) Test like you fly to ensure success: After extensive testing on the ground in “Flight Like” scenarios EFT-1 successfully tested Orion in real flight environments, which could not be duplicated in ground simulations. The systems were subjected to the most critical crew safety requirement with the same rigors they will see when carrying humans. Systems verified included: thermal protection system, hardware separation events and the parachute system. This was a 100% mission success. 87 EFT-1 flight test objectives were identified in the early phases of the test development program. These objectives included verification of Orion’s subsystems ability to launch, control its trajectory with OFI (Operational Flight Instrumentation), complete all separation events, reenter the Earth’s atmosphere at 32, 200 km/hr and 2200ºC, land accurately in the Pacific Ocean and be recovered without damage. 81 of the 87 FTOs (Flight Test Objectives) were fully satisfied with six being partially met. Four of the seven FTO's were related to suspect DFI (Developmental Flight Instrumentation) performance. Two FTO’s related to the Crew Module Up-righting System were partially met, and one FTO related to structural measurements was partially met.

6) Organize for focus: Organizationally, Lockheed Martin and NASA agreed assigning a “mission director” to each test flight would allow program focus on the near term test milestones while maintaining a parallel program focus on the remaining DDT&E (Design, Development, Test, and Evaluation) efforts. EFT-1 was the first mission where this was implemented and proved to ensure the test was completed on time and within budget. This effort also saved over one year of development time for EM-1 by performing this in parallel versus chronologically.

7) Processes and reviews tailored: Since its inception the Orion program has spent significant time focusing on defining an efficient set of requirements to enable the design of Orion as well as optimize the concept of operations for a recurring program rhythm. In an effort to remain flexible the program continues to evolve the requirements based on lessons learned. On EFT-1 the program used a consolidated requirements document approach that was successful in limiting the number of requirements, individual requirements documents, and tiers of requirements documents. The team is using the success of this approach to streamline the EM requirements where possible. Requirements verifications were completed later than planned, partly because the verification work did not carry the same urgency as other launch campaign tasks. The team is looking at a more structured “waterfall” approach to prevent lower level verifications from conflicting with launch campaign activities.

8) Flexibility to accommodate change: Several program planning improvements were accomplished during the course of the program leading up to EFT-1. Improving the Orion IMS ( Integrated Master Schedule) by integrating the NASA “non-Prime” elements improved the continuity of the entire schedule past vehicle delivery. Through Monthly Orion Program Performance Review meetings, the assessments team continued to monitor the contractor performance. Data input for these reviews consisted of Integrated Master Schedule updates, CPRs (Cost Performance Reports), Financial Management Reports (533 inputs), contractor supplemental financial and schedule data, and through participation in the subsystem IPT (Integrated Product Team) meetings. The assessments team integrated these data each month to update the assessment and forecast for the EFT-1 launch date and financial position enabling program management to make rapid decisions.

9) Partnerships ensure Communication: After the President’s proposed cancellation of the Constellation program, NASA and Lockheed Martin recognized reductions needed to occur both on the government side and within Industry to keep the program intact. NASA identified all work within their scope as “Non-Prime” and all work within Industry as “Prime”. NASA and Industry were challenged with a $738.9 M reduction in funding in 2010 and needed to re-plan the entire program in anticipation of this reduction. The cost reduction initiatives they initiated have come to be known as “The streamlining of Orion” and have been used as examples of how NASA and Industry can work together to become more efficient and affordable. The continued emphasis on meeting program objectives within the government’s affordability range have resulted in a refined program plan that accomplishes all of its goals within the annual budget and without jeopardizing mission success. One example of this was the reduction of test flights from seven to four while maintaining the same requirements verifications.

10) Supply Chain must remain healthy: EFT-1 provided the Orion team the ability to exercise 80% of the supply chain that will be utilized for future production vehicles. This includes subcontractors currently spread across 42 states with 60,000 parts being received by NASA or its prime subcontractor in 3 major integration facilities. Throughout this endeavor the processes were validated, enhancements were made and opportunities for improvement identified. EFT-1 helped establish 6 key principles needed to ensure effective supply chain management:

• Centralized supply chain ownership/management offers advantages over IPT ownership

• Need for timely actionable information, including stable engineering design documentation, is mandatory

• Consistent, effective and constant communication is mandatory

• Management of the supplier certification and work load

• Manage with the tools, don’t expect the tools to manage

• Work within the system.

In summary, NASA and Lockheed Martin are taking what we have learned from EFT-1 and years of government investments to make improvements, fly again, making improvements again, and developing a spacecraft that we can proudly stand behind and say we are confident in its abilities to take humans into deep space and bring them safely home.

Some examples of Orion design changes as a result of lessons learned from EFT-1 deals with the structure of the EM.

The Orion design for future Exploration Missions experienced many design optimizations as a result of the EFT-1 flight results. The following section highlights several changes to exemplify optimizations that was realized. Note: (For more information, the reader is referred to Ref. 10).

Structures: Reduced parts and weld assemblies required on the pressure vessel include:

- Reduction from 6 to 3 cone panels, and reduction of cone section welds from 12 to 3.

- Reduction from a 3 piece welded aft bulkhead design to a single spun-formed design.

- Change to an “Apollo-gusset” design in the aft-bay to help reduce the number of separable-parts, and combine structural elements (reduced thruster pod support structures and harness support structures, etc.).


Figure 6: A simplification and reduction of structural parts has been realized by the lessons from EFT-1 (image credit: NASA, Lockheed Martin)

Propulsion: Tubing subassemblies on EFT-1 were custom fit for propulsion system integration (e.g. fit-up tube assembly, cut, face, install heaters / temp sensors, reinstall, repeat as required). On EM-1 no trim to fit will be required on the vehicle. Tubing subassemblies will be delivered in their net shape and subassembly welds will be proof & leak tested prior to delivery.

PCAs (Pressure Control Assemblies) on EFT-1 required a custom fit for propulsion system integration (similar to Tubing subassemblies). On EM-1 there will be improved packaging and attachment methods including PCA welds proof & leak checked prior to delivery.

Propellant and Pressurant Tanks on EFT-1 were difficult to integrate and perform welding operations. The EM-1 design created a new inlet / outlet orientation to ease integration and welding operations.

RCS (Reaction Control System) thrusters on EFT-1 had support struts that have been simplified to a Pod design and attachment method eliminating all struts.


Figure 7: Left: EFT-1 Roll Left Thruster, Right: EM-1 Roll Left Thruster Pods (image credit: NASA, Lockheed Martin)

TPS (Thermal Protection Systems): The Heatshield Avcoat design improvement included changing from a monolithic, individual cell injection process to a “Block Avcoat” design where the heat shield blocks could be automated in production while increasing material properties performance. The use of thermal tape that was used on the EFT-1 heatshield (and similar to Apollo) was changed to use on all backshell and heatshield surfaces for all future Exploration Missions.

Micrometeoroid and Orbital Debris Performance: There are a number of lessons learned in the realm of MMOD (Micrometeoroid and Orbital Debris) environments and analyses, which are being examined and used to influence change for the EM and beyond missions. Chief among these lessons learned is that time spent in the high orbital debris flux altitude band, approximately 650 km to 1200 km, should be minimized. The MMOD analysis performed on EFT-1 was the first such analysis of a human-rated spacecraft above ISS ( International Space Station) altitudes since man-made orbital debris has become an issue, and found the risk at these altitudes (600 km – 1600 km) to be much higher than anticipated; Apollo was too early in spaceflight history for much OD (Orbital Debris) to have accumulated yet. Post-flight inspection of the EFT-1 capsule indicated that actual MMOD exposure may have been even higher than the analyses had assessed. Based on this lesson learned, the parking orbit of EM-1 has been reduced from 3.5 hours in a high-MMOD-risk orbit (2 orbits), to half that time (limited to 1 orbit) to reduce MMOD risk. And as EM-2 trajectory trades and analysis is ongoing, avoiding these altitudes has been accepted as a prerequisite in the EM-2 trajectories. Largely anchored on this finding, other lesson learned recommendations include: increasing MMOD protection in upper-stage and other critical hardware, re-assessing window damage cause and remediation, and continued post-flight inspections and MMOD environment recommended updates based on EM flights.

Radiation Summary: Orion is the first spacecraft that addresses crew radiation protection as an integral part of the vehicle design. We are using a state-of-the-art radiation analysis process to analyze the shielding provided by the vehicle and quantify the internal radiation environment. This analysis is based on the full fidelity Orion CAD model and space radiation environment models. Due to the EFT-1 trajectory passing through the very core of the van Allen proton belts, intravehicular radiation environment was equivalent to 4-6 weeks inside ISS (in terms of cumulative exposure). Thus EFT-1 presented a valuable opportunity to validate our analysis procedure and ultimately improve crew radiation protection for future manned missions. This opportunity was materialized by flying six RAMs (Radiation Area Monitors) on EFT-1. Radiation measurements were in very good agreement with pre-flight predictions, confirming the validity of the radiation analysis approach and providing confidence in our efforts to maintain crew radiation exposure ALARA (As Low as Reasonably Achievable) consistent with NASA requirements.

An important lesson learned for electronic components radiation hardening refers to the importance of considering time variability of the environments in the Single Event Effect rate calculations. The EFT-1 proton environment varied dramatically throughout the mission. Accounting for this time variation was an essential component in selecting the appropriate level of redundancy in critical systems such as the VMC/FCMs (Vehicle Management Computer / Flight Control Modules). This lesson continues to apply to Exploration Missions. Stochastically occurringSPEs ( Solar Particle Events) may cause significant temporary increase in the radiation environment, and critical systems need to design appropriately. A related lesson learned reflects the importance of assessing timing of critical mission events with respect to the radiation environment. Environment assessments performed for EFT-1 drove modification of the mission timeline such that Avionics intensive mission events be executed outside of the core of the van Allen belts. This too is a lesson learned relevant for future missions especially in off-nominal conditions that may expose the spacecraft to high radiation environments.

EM-2 (Exploration Mission-2): EM-2 will be a crewed test flight that will be launched on an SLS and enter lunar orbit in 2022 to verify the capability of Orion to successfully launch, perform a crewed mission, and return them safely to Earth. Figure 2 depicts one option for a lunar mission. The EM-2 configuration will consist of:

• A fully functional launch abort system

• A fully functional Crew Module that includes a crew of up to four and all Cis-Lunar life support systems

• A fully functional Service Module.


Figure 8: EM-2 Design Reference Mission (image credit: NASA)


Figure 9: Technicians with Lockheed Martin, NASA’s prime contractor for Orion, are welding together the pieces of the spacecraft's pressure vessel at Michoud Assembly Center in New Orleans, LA (image credit: NASA)

ESM (European Service Module)

The ESM implements four major system functions to Orion (Ref. 2):

• provides thrust for orbital maneuvers and attitude control after upper stage/launch vehicle separation

• generates electrical power and distributes it to the ESM users and to the CM/CMA

• regulates heat for the life support and avionics equipment during the orbital phases of the mission

• stores and provides to the CMA/CM potable water, oxygen, and nitrogen.

In addition, it ensures structural spacecraft integrity during launch and in-orbit maneuvers. The ESM can also provide additional volume and other resources on select missions for accommodating science, engineering demonstrations, development test objectives, and deployment of lunar infrastructure equipment during the cruise and lunar orbit phases of lunar missions. This volume provides electrical power distribution, network access for command and control interfaces, and structures and mechanisms.

The architecture of the module has been developed based on the ATV spacecraft concept (five successful missions to the ISS),modified to cope with the different mission requirements and the man-rating approach for beyond LEO missions. 11)


Figure 10: Illustration of an ATV cargo freighter in flight with deployed solar arrays (image credit: ESA)

The resulting ESM architecture is depicted in Figure 11, for comparison. The architecture of the system and subsystems hereafter proposed is the reference design for the Lunar Sortie Mission. Changes in the architecture are expected for the other missions to tailor the configuration to mission needs, to remove unnecessary HW and to optimize the launch mass.

European Industrial Consortium: ESA entrusted the development of the ESM (European Service Module) to a consortium of European industries led by Airbus Defence and Space. The consortium of companies was selected to reuse the experience and industrial heritage of the very successful ATV (Automated Transfer Vehicle). Airbus Defence DS Germany as the Prime Contractor is responsible for all system-related work. This includes: 12)

- The overall Management of the contract

- The overall System Engineering activities

- The Management of the procurement activities

- The System Product Assurance and Safety activities

- The liaison with Lockheed-Martin (NASA prime contractor of the Orion vehicle).

Airbus DS, France is responsible for part of the system engineering, ground software, Helium pressurant tanks and simulation facility.

On Subsystem level, Airbus DS, Germany is responsible for the System Engineering, the Propulsion, Power and Avionics Subsystem Engineering as well as for GSE and AIT activities. The responsibility for the development of the other sub-systems or equipment has been distributed among European companies as follows:

TAS (Thales Alenia Space) Italy: the Structure, Thermal and Consumable Storage Subsystems, supported by the following level-2 subcontractors:

- RUAG, Switzerland: secondary structures

- SONACA, Belgium: tank bulkhead

- APCO, Switzerland: MDPS (Meteoroid and Debris Protection System)

- CRISA, Spain, TCU (Thermal Control Unit)

- Prototech, Norway: nitrogen filters

- MEWASA, Switzerland, Water tank bellows.

Dutch Space, The Netherlands: the SAW (Solar Array Wings), supported by the following level-2 subcontractors:

- SELEX SE, Italy for the Photo Voltaic Assemblies

- RUAG, Switzerland: deployment dampers.

Airbus DS, Germany: the propellant tanks, Propulsion Drive Electronic and reaction control thrusters.

RUAG, Switzerland: the SADA (Solar Array Drive Assembly) composed of the mechanism and electronic unit.

SELEX SE, Italy: the PCDU (Power Conditioning and Distribution Unit)

Thales Alenia Space, Belgium: PRU (Pressure Regulation Unit)

Antwerp Space, Belgium: the Electrical Ground Support Equipment Front Ends, supported by the following level-2 subcontractors :

- Clemessy, France

- Rovsing, Denmark.

APCO, Switzerland: Mechanical Ground Support Equipment.

Latelec, France: avionics and power harness

TESAT Germany and Alter, Spain: CPP (Centralized Parts Procurement) scheme for EEE (Electrical, Electronic and Electromechanical)-parts.

Equipment suppliers encompasses Vacco (US), Moog (US), Sofrance (F), Cobham (US), Vivace (US).


Figure 11: Illustration of the ESM (European Service Module) without radiators and MDPS, image credit: ESA, Airbus DS

Physical architecture: The ESM is a cylindrical unpressurized module which interfaces at its bottom to the SA and at its top to the CMA. The OMS-E (Orbital Maneuvering System -Engine), i.e. the main engine, protrudes into the SA. Equipment on the tank platform is also allowed to protrude into the CMA. The total height of the ESM is 4.0 m.

The cylindrical shape is defined by the external radiators which enclose the body of the ESM. The function of the radiators is twofold, i.e. to radiate heat, and to serve as the first barrier of the MDPS (Micrometeoroid and Debris Protection Subsystem ). Mounted to the back side of the radiators are Nextel and Kevlar blankets which serve as the second barrier. The externally mounted RCS (Reaction Control System) pods and SAWs (Solar Array Wings) must be designed such that these respect the Orion SAJ allowable envelope.

The internal accommodation of the ESM subsystem equipment is highly dependent to the primary structure architecture, based on seven separate bays for accommodation, six located circumferentially about the central bay. The pressurant tanks are accommodated in the center bay. The four largest bays are used for the accommodation of the propellant tanks which dominate the available volume. The remaining volume provides accommodation to the avionics equipment, CSS (Consumable Storage Subsystem) water tanks, harnessing and tubing.

The top surface of the ESM is dominated by the protruding tank domes for the propellant subsystems, one of the helium pressure tanks, the four tanks for Oxygen and Nitrogen, and the Flow Control Assembly for the active cooling subsystem. These elements protrude into the CMA, while maintaining a specific minimum distance to the CM Heat Shield. For these elements above the tank platform, the CMA provides the MDPS protection.

The lower surface is dominated by the OMS-E, which serves as the main engine of the ESM, and the eight auxiliary thrusters. Within the lower platform, a panel is incorporated through which the UPC (Unpressurized Cargo) is installed, and optionally ejected.

Total launch mass

13,500 kg for Lunar Mission, including 8600 kg of usable propellant, 240 kg of potable water, 30 kg of N2 and 90 kg of O2


- ∅=5.2 m (with solar wings stored), L=4 m, deployed solar array span: 19 m
- ESM L is actually ~2 m, considering the primary structure only, but reaches up to 4 m adding the protrusions of the main engine toward the SA and the propellant / gas tanks toward CMA


380 kg (max), maximum volume of 0.57 m3

Solar array power

11.2 kW


- 1 main engine, ca. 30 kN
- 8 auxiliary thrusters, each 490 N
- 24 RCS (Reaction Control System) thrusters, each 220 N

Table 3: ESM characteristics for Lunar Missions

Functional architecture: Orion functionalities are generally shared between ESM and CMA/CM. Functional Chains gather equipment of the ESM which participate to a same service provided by Orion for the accomplishment of its mission.

Figure 12 depicts the overall avionics subsystem architecture and interfaces. The interface to the SLS launcher is depicted on the left side of the drawing, and the CM and CMA (labeled as SM-CM I/F Adapter) are on the right side. The main link with Orion CM on-board computers is the ODN (On-board Data Network), based on a time-triggered Ethernet solution. This interface ensures the connection of all ESM avionics to the on-board computers and allows the ESM to receive commands and to deliver monitors.

Few discrete lines ensure the independent command of ESM power subsystem electronics, allow to acquire signals from 8 sun sensors used as back-up AOCS sensors and allow the transfer of data acquired from the development flight instrumentation.

The four SAWs (Solar Array Wings) ensure a maximum electrical power production of 11.2 kW, to cope with a CMA/CM power demand of maximum 7.3 kW to be respected with one wing failed.

Four power buses allow powering to / from the CMA/CM depending on mission phases. Additional and independent power lines are provided for the wireless cameras installed on top of SAWs.

Finally, a dedicated pass-through harness connects the CMA to the SA/SAJ and launcher to allow transfer of monitoring data and separation commands.


Figure 12: ESM functional architecture (image credit: ESA, Airbus DS)

ESM Layout:

The ESM provides translational and 3-axis attitude control for the spacecraft, stores consumables for the crew module and provides power via the solar arrays. The ESM is also being designed to carry cargo. The main subsystems of the ESM are: 13)

• Structure Subsystem

• TCS (Thermal Control Subsystem)

• CSS (Consumable Storage Subsystem)

• PSS (Propulsion Subsystem)

• EPS (Electrical Power Subsystem)

• Avionics Subsystem


Figure 13: Top view of the ESM and its elements (image credit: ESA, Airbus DS)


Figure 14: Illustration of the ESM architecture and principal layout of main elements (image credit: ESA, Airbus DS)

Structure subsystem: The ESM astructure consists of the following major elements:

• Primary structure

• Secondary structure

• MDPS (Meteoroid and Debris Protection).

The primary structure transmits the SLS launch loads to the upper composite composed of the CMA, the CM, and the LAS, then supports the upper composite aerodynamic and inertial loads as well as the ESM inertial loads generated by the ESM internal equipment. The design is based on a shared load path between the ESM and the external SAJ fairings. The objective is to minimize the loads applied on the ESM mechanical structure in order to optimize its mass which is propelled all along the mission, whilst the SAJ capability is sized to the extent possible by the main launch phase, since the SAJ mass is jettisoned early during the launch. The primary structure is composed of:

• 6 longerons (machined aluminum) linked to the CMA frame and six pyronuts that separate the ESM from the Spacecraft Adapter

• Tank bulkhead (machined aluminum) supporting the four propellant tanks, as well as the gas delivery CSS tanks, ensuring the main link between the CMA lower interface ring and the rest of ESM structure.

• "Radial" shear webs and internal "square" webs assembly (composite sandwich panels), housing most of the ESM equipment, including water tanks and SAW support frames and propulsion high pressure system. It forms the ESM core attached to the tank bulkhead, longerons and lower closeout panels. The main engine is attached to the central square tube panels via struts transmitting the thrust.

• Lower Platform (machined aluminum) on which the equipment is connected: OMS-E main engine, auxiliary thrusters supports, RCS pods supports, SAD (Solar Array Drive) mechanism, and PIE (Propulsion Isolation Equipment).

• MDPS covers and aft closure panels to protect the ESM from the MMOD (Micrometeoroid and Orbital Debris) environment.

The secondary structures support the ESM equipment carrying the inertial and dynamic loads of the equipment during launch and transmitting in-orbit thrust and inertial loads.

The MDPS is partly metallic and partly composed of Nextel reinforced MLI (Multi-Layered Insulation). Debris and meteoroid particles with velocities up to 24 km/s hit the outer wall, forming a cloud of lower energy particles which are then contained by the inner wall, preventing any penetration of the ESM.


Figure 15: Primary and secondary structures (image credit: ESA, Airbus DS)

TCS (Thermal Control Subsystem): The TCS includes an ATCS (Active Thermal Control Subystem), a PTCS (Passive thermal control Subsystem) and the TCU (Thermal Control Unit).

11) ATCS (Active Thermal Control Subystem): The ATCS is designed to collect the thermal loads from the CM and from the ESM powered equipment and to reject them toward the space radiative sink. The ATCS architecture is based on a Single-phase Fluid Loop Architecture using the HFE-7200 coolant to collect and to transfer the heat loads from both ESM avionics (via cold plates) and CM (via Inter-Loop Heat Exchanger) and to reject them through specific body mounted radiators. The ATCS is composed of two fully independent loops working simultaneously (hot redundancy approach). The schematic of the ATCS architecture is presented in Figure 16.

Each ATCS loop is composed by the following main components:

• 1 Radiator Assembly commonly used for both loops and composed of 4 full height radiators and 2 split radiators (with lower part not removable) mounted in serial configuration

• 1 CP (Cold Plate)

• 2 online APSBs (Absolute Pressure Sensor Blocks)

• 1 wet on-line TSB (Temperature Sensor Block)

• 1 FCA (Fluid Control Assembly) including redundant pumps with relevant passive accumulator and a TWMV (Three-Ways Modulating Valve)

• Hard/flex hoses, tees, couplings and restrictors.


Figure 16: Architecture of the ATCS (image credit: ESA, Airbus DS)

The FCA is controlled by the TCU to provide constant mass flow rate inside the loop. In particular two flow rate set points are foreseen, one for nominal operation and one for contingency (with only one loop operative). The FCA also includes the TWMV, controlling the temperature at the ESM-CMA interface.

The external surface of the radiator panels is coated with a specific paint characterized by the following thermal-optical characteristics:

• Alpha (α) = 0.2

• Emissivity (ε) = 0.8.

The Cold Plates are devoted to collect the entire thermal load from the ESM avionics boxes. Their design is constituted by a stainless steel channelling enclosed in an aluminum casting acting as a plate in direct contact with the thermally active unit. Different Cold plate sizes, to satisfy the different configuration needs, are foreseen.


Figure 17: Photo of a sample radiator panel (image credit: ESA, TAS)

12) PTCS (Passive Thermal Control Subsystem): The PTCS provides the thermal control of ESM hardware (propulsion, CSS, power and avionic items) and reduces the temperature gradients and minimize heat flows through the internal elements. The PTCS has two main components, heaters (with thermistors and wire heater) and insulation (MLI thermal blankets, including some specific high temperature MLI blankets, for thrusters and engine nozzle thermal impingement protection).

The MLI protects the internal parts against the external environment and heater lines compensate the heat leaks toward space. Different MLI typologies, in terms of composition, have been identified for the different applications on the ESM. The MLI composition mainly depends on exposure or not to the space, geometry & fixation interfaces and exposure to thrusters plume flux and nozzle radiation.

Two cold redundant heater lines managed by the TCU assure thermal control and temperature uniformity in the Orion internals and for the local thermal control of specific items. In addition, heater lines managed by thermostats and powered by the PCDU (Power Control and Distribution Unit) provide a further redundancy to the environmental control function.

13) TCU (Thermal Control Unit): The TCU is designed to ensure the management of the TCS and of the CSS.

For the ATCS, the TCU acquires the various parameters from the ATCS sensors, monitors and commands the ATCS valves, and issues commands to the FCA (Flow Control Assembly).

For the PTCS, the TCU commands the heater chains and monitors the thermistors. It operates according to activation and de-activation thresholds defined and modified by the CM on-board computers, while ensuring bus interface and power supply logic.

For the CSS (Consumables Storage Subsystem), the TCU commands the valves and monitors their position. It also monitors the pressure and temperature parameters in the subsystem to support the system FDIR (Failure Detection, Isolation and Recovery).


Figure 18: Layout of the TCS (Thermal Control Subsystem), image credit: ESA, Airbus DS

CSS (Consumable Storage Subsystem): The CSS provides potable water, oxygen and nitrogen to the CM. It can also provide water for the sublimator located in the CMA via a dedicated kit composed by its own tank assy and distribution system, to be installed optionally for specific missions. It consists of the following major elements:

• WDS (Water Delivery Subystem)

• GDS (Gas Delivery Subsystem)

The architecture of the WDS is composed of the following components:

• Water tanks (metal bellow technology)

• Water on/off valves, (isolation valves)

• Temperature and quantity sensors

• 2 distribution lines towards the CMA I/F to supply water for the different CM/CMA needs.

The architecture of the GDS is composed of the following components:

• Gas tanks

• Gas pressure regulators

• Gas on/off valves, (isolation valves)

• Gas relief valves

• Temperature and pressure sensors

• Hydrophobic filters upstream the water tanks

• Distribution lines towards the CMA I/F to supply oxygen and nitrogen

• Distribution lines towards CMA I/F for GDS filling on ground from the GSE.

In the case of a configuration with WSK (Water Sublimator Kit) a set of 3 additional water tanks is introduced and interconnected to the others tanks and lines of CSS.


Figure 19: Layout of the CSS (image credit: ESA, Airbus DS)

PSS (Propulsion Subsystem): The propulsion subsystem design has to cope with a complex mission scenario. It includes three different types of engines / thrusters. Each of these thrusters utilizes the same propellants: MON-3 (Mixed Oxides of Nitrogen) as oxidizer and MMH (Monomethylhydrazine) as fuel.

The single Main Engine, which is one of the Shuttle OMS-E engines (27.7 kN), is delivered by NASA as GFE (Government Furnished Equipment) and will be used during ascent abort and trans-earth injection maneuvers as well as orbit change maneuvers. This engine is gimballed with an amplitude of ± 7° around both axes (pitch and yaw). The actuation is performed by the TVC (Thrust Vector Control).

The 8 auxiliary thrusters which are similar to those used on ATV (490 N) are used during ascent abort and launcher separation together with the main engine. They are also used as backup to the main engine for trans-earth injection and for trajectory correction maneuvers.

The 24 RCS thrusters which are the same as used on ATV (220 N) provide the impulse necessary for attitude control, small maneuvers and forced translation during Rendezvous and Proximity operation. These thrusters are accommodated into six pods. Two pods are composed of four roll thrusters, placed along the ESM lateral surface under the CMA, while four other pods are composed of four thrusters, placed along the ESM lateral surface under the level of the first four pods. Each propellant type is stored in two propellant tanks, both sets of propellant tanks being arranged in a series configuration.

The propellant distribution comprises several electromechanical valves for propellant isolation and pressure transducers interconnected via pipes. The assembly ensures isolation of the engine / thrusters from the propellant tanks during launch, docked phase to the ISS and other mission events where it becomes necessary to isolate the engine / thrusters from the propellant storage. The propellant distribution network provides the connections between the propellant tanks and the isolation valves and then onwards to the thruster assemblies. Fill and Drain Valves and the related access lines are used during ground testing and for loading and unloading of the propellant and pressurized tanks. They are located in the CMA to enable access even after the SAJ around the service module has been installed.

The propulsion subsystem is controlled by the PDE (Propulsion Drive Electronics) which handles all nominal propulsion related commands issued by the CM and provides feedback via the CMA PDUs (Power Distribution Units) and the PDUs to the vehicle management computer interface and the ESM network. The PDE controls all thrusters, the TVC and the associated valves, instrumentation and leakage detection.

The PRU (Pressure Regulation Unit) controls and monitors the operation of the pressure regulation valves, based on set points defined and modified by the on-board computers. The EPR (Electronic Pressure Regulation) selected for ESM has the advantage to optimize the pressure of propellant and oxidizer according to the engine in operation, at the price of an increased development risk for this function.

The EPR of the propulsion system propellant is a new technology for the European industry. The ATV design featured a mechanical pressure regulation like the propulsion system of the Shuttle OMS-E engine. The electronic pressure regulation allows a better control of the pressure, hence the fuel and oxidizer consumption is enabling to reduce propellant margins and the overall mass at launch. Airbus DS decided to venture in that new technology as a result of a trade-off taking into account the positive results obtained by Lockheed-Martin in breadboard testing. However, in the development of a new technology there is always the risk of not being successful especially if the development time is constrained.

To mitigate the impact to the project in case of unsuccessful development, it was decided to ensure that reverting to mechanical pressure regulation would be possible with minimum schedule impact. NASA provided Shuttle mechanical pressure regulators and valves to VACCO, the original manufacturer and Airbus DS ordered tests to ensure the hardware would satisfy the performance required for the ESM. Breadboard testing of the electronic regulation performed in Europe up to now delivered promising results and the probability of having to revert to mechanical pressure regulation is becoming more remote.


Figure 20: Layout of the propulsion subsystem (image credit: ESA, Airbus DS)

EPS (Electrical Propulsion Subsystem): The EPS has the function to generate the power for all modules of Orion. It manages the power provided by its 4 SAW (Solar Array Wings). The PCDU (Power Control and Distribution Unit) provides the power I/F to the SAW and CMA, distributes electrical power to ESM users and protects the power lines.

The power generation part of the ESM EPS consists of four SAW units. Each wing is composed of three deployable CFRP (Carbon Fiber Reinforced Polymer) rigid panels covered with triple junction GaAs solar cells forming nine (9x) sections of solar cell strings. In nominal condition the SAW can supply a total 11.2 kW. Each SAW is linked to the ESM structure by a two degree of freedom SADA (Solar Array Drive Assembly). The SADA ensures the power and signal transfer from the SAW to the PCDU. It is composed of SADM (Solar Array Drive Mechanism) and a (SADE (Solar Array Drive). The SADM allows orienting the SAW in two independent axes. In the Sun-tracking mode the inner axis can swivel between -35º and +25º, while the outer axis has a continuous rotation capability (0º; +360º).

SADM of the ESM has a unique design incorporating a two axis gimbal. An inner axis provides rotation of the SAW about an axis perpendicular to the ESM longitudinal axis, and an outer axis which rotates the SAW about its own longitudinal axis. The two-axis capability is necessary for two reasons:

1) allow maximum sun tracking to meet the power requirements for particular vehicle attitudes of certain mission phases. Insufficient power is generated by the SAW with a single (roll) axis SADM not providing the avoidance capability of the shadowing effect of both the Orion vehicle on the SAW and the SAWs on each other

2) insure the structural integrity of the SAWs under injection maneuvers. For the trans-lunar injection performed with the upper stage of the Space Launch System rocket, actually the iCPS (interim Cryogenic Propulsion Stage), the arrays are canted backwards to sustain in deployed configuration the 1 g acceleration load. For the trans-earth injection performed with the ESM main engine, the acceleration is less severe and the arrays have to be canted forwards to prevent damages from the OMS-E engine plume while minimizing the load on the SAWs.

The SADM also allows repositioning (canting) of the SAW to reduce the loads on the SAW and SADM during the different Orion orbital maneuvers. At TLI (Trans-Lunar Injection), a 0.5 g acceleration is generated by the iCPS engine and at LOI (Lunar Orbit Insertion) and TEI (Trans-Earth Injection) a 0.3 g deceleration is generated by the OMS-E engine.

As shown in Figure 21, in order to reduce these loads to an acceptable level, the SAWs need to be repositioned by the SADM. In TLI, the SAWs are thus canted during the maneuver to inner axis = - 60º / outer axis = 0 º. In LOI/TEI, the SAWs are canted to inner axis = +55º / outer axis = 0º.


Figure 21: Orion vehicle with ESM SAW canting angles (-60º / 0º @ TLI, +55º / 0º @ LOI/TEI), image credit: ESA, Airbus DS

The EPS distributes the generated power to the CMA/CM through four independent 120 V busses. The power interfaces of the PCDU protect each unregulated bus from overload or short circuit failures on feeder busses outside the PCDU. They are implemented with power devices connected in parallel and independently operated for power flow from PCDU to CMA PDU, plus a number of power diodes for power flow from CMA PDU to PCDU.

Avionics Subsystem: The high-level management of the vehicle and its functions is performed at the level of the Orion on-board computers. The ESM is controlled and monitored by specific electronic controller units. All units are connected via the ODN (Onboard Data Network) to the CMA/CM. All vehicle control and management software resides in the CM computers. The ODN is a three plane TTGbE (Time Triggered Gigabit Ethernet),1000Base-CX, according to standard SAE AS6802.

The Time-Triggered Gigabit Ethernet ODN provides a set of time-triggered services implemented on top of standard IEEE802.3 Ethernet. It provides the capability for deterministic, synchronous, and congestion-free communication, unaffected by any asynchronous Ethernet traffic load. By implementing this standard in network devices (network switches and network interface cards), Ethernet becomes a deterministic network. This means that distributed applications with mixed time-criticality requirements (e.g., real-time command and control, audio, video, voice, data) can be integrated and coexist on one Ethernet network.

Each of the ESM controller units is connected via a SNIC (Standard integrity Network-Interface Card), according to Honeywell ICD8273722, to the LAN switch located in the CMA. The SNICs have three ports for two failure-tolerant communication on three network redundancy planes.

Development: The challenging schedule of the program, with the ESM delivery planned for early 2017 and the EM-1 launch planned for 2018, is influencing the way the ESM is verified. Qualification has often to run in parallel to EM-1 flight model manufacturing and integration, bringing risk to the program. This risk is carefully monitored and risk reduction strategies are in place to ensure the program can proceed smoothly. The ESM verification is mostly accomplished at module level. A limited number of verifications is planned on the EM-1 flight model.

- The system PDR (Preliminary Design Review) was successfully concluded in the summer 2014.

- The system CDR (Critical Design Review) is scheduled for the end of2015 and will conclude with the board in February 2016.

• The decision to include an International Partner in the development of Orion is beneficial for NASA, enlarging the cooperation on human explorations and strengthening the international partnership.

• ESA also benefits of the ESM program because it allows to retain in Europe the experience acquired with ATV program, to participate to the exploration endeavour, and to develop additional capabilities for use toward future ESA missions.

• Both NASA and ESA, together with their industrial partners, are committed to that goal of achieving the program objective in spite of the complex interface management needed and of the challenging schedule.

Table 4: Summary of key aspects for an international partnership in the Orion program

Development status of Artemis I, formerly Orion EM-1 (Exploration Module-1) and ESM (European Service Module)

• October 13, 2021: The second European Service Module for NASA’s Orion spacecraft is on its way to USA. It is the last stopover on Earth before this made-in-Europe powerhouse takes the first astronauts around the Moon on the Artemis II mission. 14)

- An Antonov aircraft sent the module across the Atlantic in a custom-built container this morning from Bremen, Germany. Upon arrival at the Kennedy Space Center in Florida, the second European Service Module (ESM-2) will be connected to the crew module. Together they form the Orion spacecraft.


Figure 22: An Antonov aircraft sent the second European Service Module for NASA’s Orion spacecraft across the Atlantic in a custom-built container from Bremen, Germany, on 13 October 2021. It is the last stopover on Earth before this made-in–Europe powerhouse takes the first astronauts around the Moon on the Artemis II mission. Upon arrival at the Kennedy Space Center in Florida, the second European Service Module (ESM-2) will be connected to the crew module. Together they form the Orion spacecraft (image credit: ESA, A. Conigli)

- The service module is a critical element for Orion – it provides propulsion, power and thermal control and will supply astronauts with water and oxygen.

- With parts made in ten countries in Europe, there is one element that returns to American soil after testing in Germany: the service module’s main engine is a refurbished engine from Space Shuttle Atlantis that will steer the spacecraft on its way to the Moon.

- Extensive testing awaits before integration with the launcher. Artemis II will be the first crewed mission to the Moon since the Apollo 17 mission in 1972.

We are going

- “This is another big step forward to the Moon for ESA. Our astronauts will fly to the lunar Gateway aboard Orion. Meanwhile, we are working to have ESA astronauts on the Moon by the end of this decade, and keep our sights on Mars as the horizon goal of human exploration,” says David Parker, ESA’s director of human and robotic exploration.


Figure 23: Integration of the European Service Module 2 (ESM-2) for Orion, the American crewed spacecraft for the Artemis program, at Airbus' Bremen site (image credit: Airbus)

- ESA is delivering up to six modules to NASA, with three more currently under negotiation for the lunar Gateway. Airbus is ESA’s prime contractor for building the first six service modules.

Full Moon schedule

- The Kennedy Space Center is humming with lunar activity this week. For the first time, three Orion spacecraft will be there at various stages of assembly and integration.

- The first Orion spacecraft will be integrated on top of the Space Launch System rocket in its final preparations for the uncrewed Artemis I mission. The European Service Module will take the spacecraft more than 64,000 km beyond the Moon in a test flight to demonstrate its capabilities.

- “Agencies, industry and teams from different continents are working around the clock in a tremendous international effort to take this complex spacecraft to the launch pad,” said Cathy Koerner, NASA Orion program manager, during a press event held by Airbus last week.

- Two arrivals mark the lunar week on site: ESM-2 and the main pressure vessel for Artemis III, which will see the first woman and next man setting foot on the Moon.

- In Europe, the third European Service Module is at the start of its integration phase where equipment dummies, brackets and harness will be added to the structure.

• October 6, 2021: The European Space Agency is playing a vital role in humankind’s return to the Moon. In a few months NASA will launch Artemis I from the Kennedy Space Center. The uncrewed mission will carry NASA’s Orion spacecraft incorporating ESA’s European Service Module (ESM-1), built and tested by Airbus Bremen, in Germany, with the help of 10 European nations. ESM-1’s main engine and 32 thrusters will propel Orion into orbit around the Moon and return it to Earth. 15)

- As Artemis I prepares for launch, the second European Service Module (ESM-2) is about to ship to the US with ESM-3 also currently under construction. The second Artemis mission, however, has a crucial difference: it will carry four astronauts for a lunar flyby. ESM-2 will provide propulsion, power, oxygen, water and life support as well as controlling the temperature in the orbiting crew module. ESM-3 will go one step further and put the first person on the Moon for 50 years.

Figure 24: This film features soundbites from: Matthias Gronwoski, Chief Engineer Orion ESM, Airbus; Rachid Amerkrane, Project Manager Orion ESM, Airbus; Philippe Deloo, ESM Program Manager, ESA (video credit: ESA)

• May 14, 2021: The pieces are stacking up for the launch of Artemis 1 mission around the Moon and back. The massive Space Launch Systems (SLS) rocket that will launch the first crewless test flight of the Orion spacecraft, powered by the European Service Module, is being integrated at the Vehicle Assemble Building at NASA’s Kennedy Space Center in Florida, USA. 16)


Figure 25: Visible in this image are the twin solid fuel rocket boosters, now fully stacked atop the mobile launcher. The boosters will be mated with the rocket’s 65 m tall core stage that recently barged in to Florida aboard the Pegasus barge on 27 April after successful testing at NASA’s Stennis Space Center in Mississippi (image credit: NASA, J. Blair)

- Once the rocket stages are ready to go, the Orion spacecraft and additional flight hardware are next up for integration.

- Since our last Orion and the European Service Module update for Artemis I, the spacecraft has moved, from the NASA Kennedy Space Center’s Neil Armstrong Operations and Checkout facility, a few kilometers down the road to the Multi Payload Processing Facility. The names of these buildings give the game away. The first Orion spacecraft has been checked out and is ready for the next step on the road to space: processing for launch.

- Fuelling was completed on 1 April, after which the system will be serviced in high pressure helium that serves as a pressurization agent to the European Service Module propellant tanks, ensuring the correct pressure at the engine inlets.

- Eventually, the spacecraft will be hoisted to the top of the fully stacked SLS rocket.

- Read more updates on the Orion blog.

• April 20, 2021: Employees across NASA’s Katherine Johnson Independent Verification & Validation Facility (IV&V) are working on software safety and assurance for the Artemis program, and efforts won’t end with the next steps on the Moon. 17)

- The Artemis program includes a series of robotic and human exploration missions in collaboration with commercial and international partners to establish sustainable exploration. From there comes the next giant leap – sending astronauts to Mars.

- A lot has changed since 1969, but traveling to the Moon is still in NASA’s sights with the Artemis program, and this time around the IV&V Program is here to help, according to Program Director Gregory Blaney.

- “Software is a critical element in the operation of every Artemis project. Many activities are conducted in space needing exact timing and precision while operating in a harsh environment; meaning, they must work precisely or the mission will fail,” he said. “Putting humans back on the surface of the Moon to explore and perform science is one step closer and practice for sending humans to Mars.”

- Expanding human presence farther into the solar system is part of the agency’s Moon to Mars exploration approach, which will help NASA and our partners learn more about the fundamental aspects about how planets and planetary systems form.

- Applying what we learn is key to expanding on what comes after Artemis. IV&V’s Artemis Program leaders say the missions provide a chance to work out ways of operating and solving challenges that are applicable to Mars missions while we’re relatively close to home.

- With that comes astronaut safety, and according to IV&V’s Artemis Program Manager Michael Facemire, almost everything critical to Artemis mission safety and success is also critical to astronaut safety.

- “Astronaut safety is on our minds throughout our work. Astronauts will not fly Artemis missions until at least Artemis II; however, a key objective of Exploration Flight Test-1 (EFT-1) and Artemis I is to make sure the systems and software are safe for the astronauts for crewed Artemis missions and beyond,” he said. “As we have worked EFT-1 and are working Artemis I, we are considering how the EFT-1 and Artemis I system software capabilities will be used in future Artemis missions, making sure that our assurance appropriately considers implications for astronaut safety in crewed missions.”

- Looking ahead, IV&V is contributing to the Gateway outpost around the Moon, which will support human and scientific exploration in deep space. It is a vital part of sustainable lunar exploration and could serve as a model for future missions to Mars. In addition, the powerful Space Launch System rocket that will lift the Orion crew vehicle that will carry the crew to space will evolve over future missions and allow the humans to travel deeper into space than ever before.

- IV&V’s Artemis program is continuing to put in efforts that accomplish what the mission needs today and what it will lead to in days and years to come, according to IV&V project leadership.

- As IV&V experts continue supporting the Artemis mission and the safety and assurance of its various components and software, Blaney offers reminders of how much innovation and discovery is in store for the program, agency, and space exploration in general.

- “NASA will gain critical knowledge and experience from Moon exploration activities which will enable future and further out explorations to Mars or beyond,” he said. “When doing things that have never been done before with humans in such harsh and different environments, you must explore and learn, adjust and advance, so you can explore further the next time.”


Figure 26: Illustration of the Gateway, an outpost orbiting the Moon that will provide vital support for NASA's Artemis missions (image credit: NASA)

• April 8, 2021: When NASA’s Space Launch System (SLS) rocket and Orion spacecraft lift off from the agency’s Kennedy Space Center in Florida on the Artemis I mission, the amount of data generated by the rocket, spacecraft, and ground support equipment will be about 100 MB/s. The volume and speed of this information demands an equally complex and robust computer system to process and deliver that data to the launch team and corresponding mission systems in real time. 18)


Figure 27: Members of the Artemis I launch team participate in a countdown simulation inside the Launch Control Center’s Firing Room 1 at NASA’s Kennedy Space Center in Florida on Feb. 3, 2020. A team of nearly 100 engineers from Orion, Space Launch System and Exploration Ground Systems came together to work through a series of simulated challenges, as well as a final countdown procedure. Artemis I will be the first integrated test flight of the Orion spacecraft and SLS rocket – the system that will ultimately land the first woman and the next man on the Moon (image credit: NASA, Kim Shiflett)

- That computer software and hardware – called the spacecraft command and control system (SCCS) – is now certified for use on Artemis I. Shawn Quinn, director of NASA Engineering at Kennedy, and the KSC Engineering Design Certification Review Board signed off on the system at the conclusion of a recent design certification review for SCCS.

- The system is the electronic hub where information traveling to and from the SLS core stage, the rocket's Interim Cryogenic Propulsion Stage (ICPS), Orion, ground systems, and the operators inside the firing room intersect. During loading and launch, the software will process up to 575,000 changes per second.

- "We're flying three vehicles in parallel – Orion spacecraft, ICPS, and SLS core stage – and SCCS needs to be able to communicate with all three simultaneously," said Mike Van Houten, the Launch Control System project manager in the Command, Control and Communications organization within EGS. “While we're ‘talking’ with the spacecraft and vehicles, we're also receiving data from Kennedy’s ground systems – programmable logic controllers, subsystems in the field, and equipment on the mobile launcher.”

- Making sense of that much data is as complex as efficiently managing the real time movements of hundreds of thousands of people within a large metropolitan area, Van Houten said.

- “Each bit of telemetry data coming from a different interface is like a person arriving into the city via a plane, train, automobile, bus, or ferry,” he explained. “Just like each person, each bit of data needs to arrive at a unique destination, whether that’s a display, application, or recording. And all the movements have to be synchronized so data arrives exactly where it should be in the quickest timeframe possible.”

- All this information is integrated into the displays shown on consoles throughout Firing Room 1 and Firing Room 2 inside Kennedy's Launch Control Center, enabling Operators to make informed decisions on how to continue the activity in progress.

- Comprising a mix of custom-built software and off-the-shelf products, the SCCS was developed specifically to manage processing and launch operations for Artemis missions. As Artemis began to take shape, NASA’s Exploration Ground Systems (EGS) team and its lead contractor, Jacobs, advanced the effort to develop a robust, updated system.

- The certification marks the end of the system’s development and signals the start of the “sustaining” phase of the project for Artemis I. Moving forward, countdown and launch simulations performed by the EGS-Jacobs team will help train the launch team and fine-tune the SCCS.

- During these simulations, Operators step through prelaunch checklists to practice the procedures for liftoff and ascent. Some simulations focus on specific operations while others walk the team through critical portions of the countdown. Each rehearsal allows the team to gather useful data to refine the system.

- “The SCCS system engineering and performance teams evaluate the data after each simulation to ensure the system is performing per specifications and no unexpected errors were triggered,” Van Houten said. “It gives the SCCS team an indication of where we need to tackle problems before the next sim or operational event.”

- Lessons learned from launching the uncrewed Artemis I will help SCCS developers identify process, performance, and technical changes needed for future missions. The developers will focus on capturing new requirements and the expectations of stakeholders such as the Artemis I launch director, firing room operators, the ground support equipment team, the ground to flight application software team, the model and simulation team, and the launch training team. This information will help the SCCS developers make system upgrades to support the crewed Artemis II flight test and future missions.

- Under the Artemis program, NASA is leading the way in human exploration of deep space with increasingly complex missions to explore the Moon and prepare for future missions to send astronauts to Mars.

• November 24, 2020: NASA has stacked the first piece of the Space Launch System (SLS) rocket on the mobile launcher in preparation for the Artemis I launch next year. At NASA’s Kennedy Space Center in Florida, engineers lowered the first of 10 segments into place Nov. 21 for the twin solid rocket boosters that will power the first flight of the agency’s new deep space rocket. Artemis I will be an uncrewed flight to test the SLS rocket and Orion spacecraft as an integrated system ahead of crewed flights to the Moon with the Artemis program. 19)


Figure 28: The solid rocket boosters are the first components of the SLS rocket to be stacked and will help support the remaining rocket pieces and the Orion spacecraft (image credit: NASA/Kim Shiflett)

- The booster segments arrived by train at the Florida spaceport in June from Northrop Grumman’s manufacturing facility in Utah to undergo final launch preparations. Stacking operations began Nov. 19 with engineers transporting a booster segment from the Rotation, Processing and Surge Facility to the 525-foot-tall Vehicle Assembly Building (VAB).

- Each booster consists of five segments and will provide 7 million pounds of thrust for the liftoff from Launch Pad 39B. When assembled, each booster will be about half the length of a football field, and together they will generate more thrust than 14 four-engine jumbo commercial airliners. Once stacked, the SLS rocket will stand taller than the Statue of Liberty and have about 15% more thrust at liftoff than the Apollo program Saturn V rocket, making it the most powerful rocket ever built.

- “Stacking the first piece of the SLS rocket on the mobile launcher marks a major milestone for the Artemis Program,” said Andrew Shroble, an integrated operations flow manager with Jacobs. “It shows the mission is truly taking shape and will soon head to the launch pad.”

- The solid rocket boosters are the first components of the SLS rocket to be stacked and will help support the remaining rocket pieces and the Orion spacecraft. Over the next several weeks, workers will use an overhead crane that can hold up to 325 tons (the weight of about 50 elephants), to lift the remaining segments one by one and place them carefully onto the 380-foot-tall mobile launcher, the structure used to process, assemble, and launch the SLS rocket. The cranes are precise enough to lower an object onto an egg without cracking it.

- The first booster segments to be stacked are the bottom sections known as the aft assemblies. These house the system that controls 70% of the steering during initial ascent of the rocket. This section includes the aft motor segment and skirt, and the nozzle that directs the hot gas leaving the motor. After stacking the other four segments, the final pieces of the boosters are the forward assemblies, which include the nose cone that serves as the aerodynamic leading edge of the boosters. The forward assemblies will attach to the core stage when it arrives next year.

- Under the Artemis program, NASA aims to land the first woman and the next man on the Moon in 2024 and establish sustainable lunar exploration by the end of the decade. SLS and Orion, along with the human landing system and the Gateway in orbit around the Moon, are NASA’s backbone for deep space exploration.


Figure 29: The Space Launch System is managed by Marshall Space Flight Center in Huntsville, Alabama (image credit: NASA)

• November 6, 2020: Technicians have finished encapsulating the European Service Module for NASA’s Orion spacecraft that will travel around the Moon on the Artemis I mission. 20)


Figure 30: Like most spacecraft Orion will be launched inside protective fairings on top of its Space Launch System rocket. The spacecraft adapter jettison fairings have now been installed that protect the European Service Module during launch and are ejected shortly after liftoff (image credit: NASA)

- The next time the ESM (European Service Module) will be visible it will be in space, when the four 7-m-long solar wings unfold to start generating power for the spacecraft. The three fairings are each around 4 m square, the size of a small room, after launch they will be blown away by small pyrotechnic explosions revealing the four solar panels and the European Service Module underneath.

- Above the European Service Module is the Crew Module where up to four astronauts will live and work on a typical two-week flight to the Moon and back. The first mission, Artemis I, will be uncrewed and is set to launch next year.

- With the spacecraft jettisonable adapters installed at NASA’s Kennedy Space Center in Florida, USA, the European Service Module will not be easily visible on Earth again, although technicians can access the module to service it and fill the tanks with fuel, helium, nitrogen and ammonia for the cooling system and other consumables.

- The final assembly activities for the spacecraft include installation of the forward bay cover, which protects the upper part of Orion including its parachutes throughout its mission, final adjustments of the main parachutes, securing and testing of electrical connections, along with closure and latching of the side hatch.

- As each area of the spacecraft is closed out, it will undergo final inspections to complete production. The spacecraft will then begin its path to the pad, including stops along the way to be fuelled and integrated with its launch abort system and, ultimately, the SLS rocket for launch.

- In December the European Service Module will be officially handed over to NASA’s launch preparation teams with ESA in a supporting role for Exploration Ground Support, during the mission and for post-flight analysis. ESA will no longer be responsible for the hardware as the spacecraft heads into final preparations for launch – a milestone for the hundreds of people involved who worked securely and tirelessly to make humankinds next-generation exploration vessel.

- Meanwhile in Bremen, Germany, work is progressing smoothly on the second and third European Service Modules that will send astronauts around and to the Moon. Technicians are currently installing the four propellant tanks for the European Service Module for Artemis II.

• October 8, 2020: On our journey forward to the Moon and on to Mars, NASA must test our technologies and capabilities to ensure astronaut safety. The Artemis I mission will be an uncrewed flight test of the Orion spacecraft that places a human-rated crew vehicle in lunar orbit for the first time since the Apollo missions of the 1960s and 70s. The mission will showcase the capabilities of both Orion and the Space Launch System (SLS), NASA’s powerful new rocket, which will launch Artemis missions from Kennedy Space Center in Florida. 21)

- Artemis I will demonstrate NASA’s networks’ comprehensive services for journeys to lunar orbit. The mission requires all three of NASA’s major networks to work in tandem, providing different communications and tracking service levels as Orion leaves Earth, orbits the Moon, and returns safely home.

- Communications services allow flight controllers in mission control centers to send commands to the spacecraft and receive data from Orion and SLS systems. Tracking, or navigation, services enable the flight controllers to see where the spacecraft are along their trajectory through space.

NASA’s Near Earth Network (NEN)

- Based out of NASA’s Goddard Space Flight Center in Greenbelt, Maryland, NASA’s Near Earth Network (NEN) consists of ground stations worldwide that provide direct-to-ground communications and navigation services. NEN stations will provide communications and navigation services during launch and navigation services at various points on Artemis I’s journey to the Moon.

- The NEN’s Launch Communications Segment (LCS) will provide critical links to both Orion and SLS during prelaunch and launch of Artemis I. Three ground stations along Florida’s space coast comprise LCS, which was designed to meet the specific needs of the SLS launch vehicle and will grow to support other missions after Artemis I.

- Specifically, the first two stations along the rocket’s flight path will provide uplink and downlink communications between the rocket and mission controllers. In the final phases of ascent, the third station will downlink high rate telemetry and video from SLS while Orion connects to the satellites in NASA’s Space Network.

- Despite the name suggesting the network’s services are limited to “near Earth,” the NEN’s navigation services extend to Orion’s journey from low-Earth orbit to the Moon and back through ground stations in Santiago, Chile, and Hartebeesthoek, South Africa.

- These NEN stations will support navigation data before and after the outbound trajectory correction burns that ensure the spacecraft stays on a path towards the Moon. The NEN will also provide navigation services during Orion’s outbound powered flyby burn that occurs at the mission’s closest approach to the Moon, setting the stage for final insertion into lunar orbit.

- For Orion’s return from the Moon, the NEN will provide navigation data for departure from lunar orbit and the return power fly-by burn that will place Orion on a course back for Earth, during which the NEN will also provide navigation services.

NASA’s Space Network (SN)

- NASA’s Space Network, also based at Goddard, can provide near-continuous communications services to spacecraft through a constellation of Tracking and Data Relay Satellites (TDRS). Located about 22,000 miles above Earth, TDRS relay data from spacecraft at lower altitudes to ground antennas. The Space Network will play a critical role during launch and low-Earth orbit phases of the Artemis I mission.

- Beginning at the launchpad, the Space Network will maintain a connection with Orion and the Interim Cryogenic Propulsion Stage (ICPS). ICPS provides the power to accelerate the spacecraft fast enough to overcome the pull of Earth’s gravity and set in on a precise trajectory to the Moon. The Space Network will continue service until Orion and ICPS leave TDRS coverage, when NASA’s Deep Space Network (DSN) takes over.

- On Orion’s return to Earth, the Space Network will facilitate communications from the final return trajectory correction burn through splashdown in the Pacific Ocean and recovery of the capsule. The return trajectory correction burn ensures Orion enters the atmosphere at just the right moment, allowing NASA to land the craft safely.

NASA’s Deep Space Network

- After handover from the Space Network, the DSN, managed by NASA’s Jet Propulsion Laboratory in Southern California, will handle communications for Artemis I beyond low-Earth orbit. This includes the mission’s outbound trajectory corrections, outbound powered flyby, return powered flyby burns, and return trajectory corrections while the NEN provides supplemental navigation data.

- The NEN and DSN tag team navigation for Orion so that engineers can employ a technique called three-way Doppler tracking. Using this method — with two ground stations on Earth in contact with Orion simultaneously, one each from NEN and DSN — NASA can triangulate Orion’s location relative to the ground stations.

- At the Moon, DSN will enable insertion into distant retrograde orbit (DRO). DRO is a highly stable orbit in which Orion travels retrograde, or opposite, from the direction the Moon travels around Earth. The DSN will maintain communications with Orion while in DRO and during the burns for DRO departure, return power fly-by, return transit and the final return trajectory correction burn, with assistance from the Space Network.

- The DSN will also help facilitate communications for all three of the mission’s CubeSat deployment stops. The CubeSats are small satellites that will be deployed along Orion’s trajectory to provide additional research opportunities for scientists and engineers. After deployment, many of the CubeSats will also communicate through the DSN.

- The networks supporting Artemis receive programmatic oversight from NASA’s Space Communications and Navigation (SCaN) program office. In addition to providing communications services to missions, SCaN develops the technologies and capabilities that will help propel NASA to the Moon, Mars and beyond.

• October 1, 2020: The new ESA logo and NASA’s ‘worm’ logo will be along for the ride on the first full mission of the powerful Space Launch System (SLS) rocket and Orion spacecraft. Teams at NASA’s Kennedy Space Center in Florida, USA, have started to apply the historic logos on the Artemis I rocket and spacecraft. 22)


Figure 31: Logos on Orion. The space agency logos for the next spacecraft to head to the Moon have been added to Orion as part of the Artemis program. ESA’s logo reflects our European nature and our pioneering activities in space. NASA’s ‘worm’ design was officially introduced in 1975 and was incorporated into many of the agency’s next-generation programs. It was retired in 1992, but made a comeback in 2020 as a new, modern era of human spaceflight becomes reality (image credit: NASA)

• September 22, 2020: Already integrated and tested with the first European Service Module that will power and propel the craft and the Crew Module, Orion has now been fitted with the adaptor cone that will connect it to the Space Launch Systems (SLS) rocket. This is one of the final major hardware checkouts before being integrated with SLS for the Artemis I launch to the Moon next year. 23)


Figure 32: There it is – the first Orion spacecraft to travel to the Moon is seen here in the Neil Armstrong Operations and Checkout facility at NASA’s Kennedy Space Center in Florida, USA (image credit: NASA)

- Earlier this month at NASA’s Kennedy, the last solar wing for Orion was unfolded, tested and folded for launch. This week, the four solar arrays will be connected to the main structure.

- Each 7 m wing are hinged at two points so they can be folded to fit inside the fairing of the SLS rocket. After launch and in Earth orbit the four wings unfold to span 19 m and swivel and rotate to collect solar energy, turning it into electricity for the spacecraft’s systems.

- Needless to say, all teams involved – NASA, ESA and the 16 companies in ten European countries supplying the components that make up humankind’s next generation spacecraft for exploration – are over the Moon.

• September 1, 2020: NASA’s Orion Program has completed the System Acceptance Review and Design Certification Review to certify the Artemis I spacecraft is fit for flight, ready to venture from Earth to the lunar vicinity, and return home for landing and recovery. 24)

- The review examined every spacecraft system, all test data, inspection reports, and analyses that support verification, to ensure every aspect of the spacecraft has the right technical maturity.

- In effect, the review gives the stamp of approval to the entire spacecraft development effort and is the final formal milestone to pass before integration with the Space Launch System rocket.

- In addition to spacecraft design, the review certified all reliability and safety analyses, production quality and configuration management systems, and operations manuals.

- Orion, the Space Launch System, and Exploration Ground Systems programs are foundational elements of the Artemis program, beginning with Artemis I, the first integrated flight test of Orion and SLS next year. Artemis II will follow as the first human mission, taking astronauts farther into space than ever before.

• August 14, 2020: Technicians at NASA’s Kennedy Space Center in Florida are working to install an adapter that will connect the Orion spacecraft to its rocket for the Artemis I mission around the Moon. This is one of the final major hardware operations for Orion prior to integration with the Space Launch System (SLS) rocket. 25) 26)


Figure 33: The spacecraft adapter cone (seen at the bottom of the stack pictured above) connects to the bottom of Orion’s service module and will later join another adapter connected to the top of the rocket’s interim cryogenic propulsion stage (ICPS). During the process to install the cone on Orion, the spacecraft is lifted out of the FAST (Final Assembly and Systems Testing) cell and placed into the Super Station support fixture (image credit: NASA, Brian Dunbar, ESA)

- Orion is NASA’s next exploration spacecraft to transport astronauts to the vicinity of the Moon and to the Gateway orbiting the Moon. The spacecraft will hold four people and send them farther than any humans have travelled from Earth.

- ESA is supplying the European Service Module for Orion, in an arrangement that stems from the International Space Station partnership. Based on ESA’s proven Automated Transfer Vehicles for supplying the Space Station, the module will provide everything to keep the astronauts alive, including oxygen, water, thermal control, electricity and propulsion.

• July 30, 2020: The second to last piece of hardware for the Artemis I test flight around the Moon has arrived at the agency’s Kennedy Space Center in Florida. The launch vehicle stage adapter (LVSA) connects the core stage of NASA’s Space Launch System (SLS) rocket to the upper stage, called the Interim Cryogenic Propulsion Stage. The cone-shaped connector also helps protect the RL10 engine housed in the upper stage, which will provide the power necessary to leave Earth’s orbit and send the Orion spacecraft on its journey to the Moon. 27)


Figure 34: NASA's Pegasus barge, carrying the launch vehicle stage adapter (LVSA) for the agency's Space Launch System (SLS) rocket, arrives at the Kennedy Space Center Launch Complex 39 turn basin wharf on July 29, 2020. Traveling to Florida from NASA's Marshall Space Flight Center in Huntsville, Alabama, the LVSA will connect the SLS core stage to the rocket's upper stage for the Artemis I launch (image credit: NASA/Isaac Watson)

- “The launch vehicle stage adapter arriving to Kennedy is significant because we have almost all of the pieces of the rocket here as we get closer to launch,” said Allison Mjoen, operations project engineer with the Exploration Ground Systems program. “We have moved from planning into implementation, and soon the rocket will begin taking shape with stacking operations.”

- Arriving at Kennedy’s Launch Complex 39 turn basin wharf, the LVSA traveled from NASA’s Marshall Space Flight Center in Huntsville, Alabama, to Florida on the agency’s Pegasus barge – a 310-foot-long vessel that has been modified to transport the largest rocket stage in the world: the SLS core stage. Technicians offloaded the LVSA and transported it to the Vehicle Assembly Building, where it will be stored until it is needed for stacking on the rocket. The core stage – made up of the forward skirt, liquid oxygen tank, liquid hydrogen tank, and the engine section containing the rocket’s four RS-25 engines – is the final piece of the rocket that will be delivered to Kennedy ahead of the Artemis I launch.


Figure 35: Technicians with NASA’s Exploration Ground Systems move the launch vehicle stage adapter (LVSA) for the agency’s Space Launch System (SLS) rocket to the Vehicle Assembly Building (VAB) on July 30, 2020, for processing. The LVSA will connect the SLS core stage to the rocket’s upper stage and will remain in the VAB until it’s time for stacking on the mobile launcher ahead of the Artemis I launch. The first in a series of increasingly complex missions, Artemis I will test SLS and the Orion spacecraft as an integrated system prior to crewed flights to the Moon (image credits: Jacobs/Tracy Yates)

- Under the Artemis program, NASA is working toward landing the first woman and the next man on the Moon by 2024. Artemis I will test SLS and Orion as an integrated system prior to crewed flights and is the first in a series of increasingly complex missions that will enable human exploration to the Moon and Mars. SLS and Orion, coupled with the Human Landing System and the Gateway in orbit around the Moon, will be the agency’s backbone of deep space exploration.

• June 16, 2020: The rocket booster segments that will help power NASA’s first Artemis flight test mission around the Moon arrived at the agency’s Kennedy Space Center in Florida on Monday for launch preparations. 28)

- All 10 segments for the inaugural flight of NASA’s first Space Launch System (SLS) rocket and Orion spacecraft were shipped by train from Promontory, Utah. The 10-day, cross-country journey is an important milestone toward the first launch for NASA’s Artemis program.


Figure 36: Twin rocket boosters for NASA’s Space Launch System (SLS) that will power Artemis missions to the Moon have arrived at the agency’s Kennedy Space Center in Florida. The two motor segments, each comprised of five segments, arrived at Kennedy’s Rotation, Processing and Surge Facility (RPSF) on June 15, 2020, by train from a Northrop Grumman manufacturing facility in Promontory, Utah. The booster segments will remain in the RPSF for inspection prior to processing until it’s time to move them to the Vehicle Assembly Building for stacking on the mobile launcher. This is the first piece of flight hardware to arrive at Kennedy by train for the Artemis program, but NASA’s Exploration Ground Systems (EGS) can expect to receive additional hardware soon, including the Launch Vehicle Service Adapter and the rocket’s core stage. NASA is working toward an Artemis I launch date in 2021, keeping the program moving at the best possible pace toward the earliest possible opportunity (image credit: NASA/Kevin O'Connell)

- “The arrival of the booster segments at Kennedy is just the beginning of the SLS rocket’s journey to the pad and onward to send the Orion spacecraft to the Moon,“ said NASA Administrator Jim Bridenstine. “Artemis I will pave the way toward landing the first woman and the next man on the surface of the Moon in 2024 and expanding human exploration to Mars.”

- Each rocket booster has individual motor segments, located between the forward assemblies and aft skirts, making up the largest single component of the entire booster. The two SLS rocket boosters, four RS-25 engines, and core stage, produce a combined total of more than 8.8 million pounds of thrust power during launch.

- “It’s an exciting time at NASA’s Kennedy Space Center as we welcome Artemis flight hardware and continue working toward the Artemis I launch,” said Kennedy Space Center Director Bob Cabana.

- Each booster segment, weighing 180 tons, is filled with propellant and outfitted with key flight instrumentation. Due to their weight, Northrop Grumman, which is the booster lead contractor, transported the segments in specially outfitted railcars to make the 2,800-mile trip across eight states to Florida’s Space Coast.

- “The fully assembled boosters for NASA’s Space Launch System rocket are the largest, most powerful solid propellant boosters ever built for flight,” said Bruce Tiller, manager of the SLS Boosters Office at NASA’s Marshall Space Flight Center in Huntsville, Alabama. “These enormous rocket motors help provide the necessary launch power for the SLS deep space rocket.”

- Now that the booster segments are at Kennedy, NASA’s Exploration Ground Systems team will prepare them for assembly and integration activities that start with offloading the segments. Teams will attach the aft segments to the aft skirts and offload and store the remaining segments from the railcars in preparation for stacking.

- “It is good to see booster segments rolling into the Kennedy Space Center,” said Mike Bolger, program manager of Exploration Ground Systems. “The team can’t wait to get started working on the boosters that will send the SLS rocket and Orion spacecraft on the first Artemis mission to the Moon.”

- The solid rocket boosters are the first elements of the SLS rocket to be installed on the mobile launcher in preparation for launch. The aft booster assemblies will be lifted on to the mobile launcher, followed by the remaining booster segments, and then topped with the forward assembly.

- Teams at Kennedy have been preparing for the arrival of the booster segments by assembling and testing the aft skirts and forward assemblies of the boosters, and practicing stacking procedures with booster pathfinders, or hardware replicas, earlier this year. NASA and Northrop Grumman completed casting in 2019 of all 10 of the motor segments for both the first and second Artemis lunar missions, and are now working on the boosters for the Artemis III mission, which will land the first woman and next man on the Moon in 2024.

- With the arrival of the boosters, the only remaining pieces of hardware for the Artemis I flight test to be delivered to Kennedy are the launch vehicle stage adapter, which connects the rocket to the Orion spacecraft and will arrive this summer, and the SLS core stage, which will be transported to Kennedy by barge after the Green Run hot fire test later this year at NASA’s Stennis Space Center near Bay St. Louis, Mississippi.

- Through the Artemis program, NASA will return astronauts to the Moon’s surface in four years. SLS, along with NASA’s Orion spacecraft, the Human Landing System and the Gateway in orbit around the Moon, will serve as NASA’s backbone for deep space exploration. SLS is the only rocket that can send Orion, astronauts, and supplies to the Moon on a single mission. We’ll explore more of the lunar surface than ever before, and collaborate with our commercial and international partners to establish sustainable exploration by the end of the decade. Then, we will use what we learn on and around the Moon to take the next giant leap – sending astronauts to Mars.


Figure 37: A train carrying the rocket motors for NASA’s Space Launch System rocket after departing a Northrop Grumman manufacturing facility in Utah for NASA’s Kennedy Space Center in Florida on June 5, 2020. The 10 booster segments will power Artemis I, the first mission of NASA’s Artemis program, to the Moon. The 180-ton booster segments are transported in specially outfitted railcars to make the 2,800-mile trip across eight states to Kennedy (image credit: Northrop Grumman)

• April 23, 2020: Before NASA’s mighty Space Launch System (SLS) rocket can blast off from the agency’s Kennedy Space Center to send the Orion spacecraft into lunar orbit, teams across the country conduct extensive testing on all parts of the system. Guiding that effort at the Florida spaceport are NASA Test Directors (NTDs).


Figure 38: NASA Launch Director Charlie Blackwell-Thompson, above, confers with Senior NASA Test Director Jeff Spaulding, left, and Test, Launch and Recovery Operations Branch Chief Jeremy Graeber in Firing Room 1 at Kennedy Space Center's Launch Control Center during a countdown simulation (image credit: NASA/Cory Huston)

- NTDs within the Exploration Ground Systems program are in charge of flight and ground hardware testing in Kennedy’s Launch Control Center firing rooms 1 and 2, where activities involved with preparing rockets, spacecraft and payloads for space can be controlled from computer terminals. They are responsible for emergency management actions, helping lead the launch team during all facets of testing, launch and recovery.

- NASA’s Artemis missions will land American astronauts on the Moon by 2024, beginning with Artemis I, the uncrewed flight test of SLS and Orion.

- “It’s certainly an amazing feeling to be responsible for setting up the building blocks of a new program which will eventually take us to the Moon, Mars and beyond,” said Senior NASA Test Director Danny Zeno.

- Zeno is leading the development of test plans and procedures that are essential to flight and ground hardware for the Artemis missions. This includes proving the functionality of flight and ground systems for the assembled launch vehicle configuration, verifying the mobile launcher arms and umbilicals operate as expected at launch, and performing a simulated launch countdown with the integrated vehicle in the Vehicle Assembly Building.

- The 14-year NTD veteran relishes his hands-on role in successfully testing and launching SLS — the most powerful rocket NASA has ever built.

- “It’s very fulfilling,” Zeno said. “What excites me about the future is that the work I’m doing today is contributing to someday having humans living and working on other planets.”

- There are 18 people in the NTD office — all of whom must undergo rigorous certification training in the management and leadership of test operations, systems engineering and emergency response. They are in charge of the people, hardware and schedule during active firing room testing.

- “The NTD office is at the center of testing operations, which will ensure that we are ready to fly the Artemis missions,” said Launch Director Charlie Blackwell-Thompson. “As we lay the foundation for exploring our solar system, the NASA test directors are on the front lines of making it happen.”

- An NTD works from a console in the firing room during integrated or hazardous testing, guiding the team through any contingency or emergency operations. They lead critical testing on Launch Pad 39B and the, the 370-foot-tall, 11 million-pound steel structure that will launch the SLS rocket and Orion spacecraft on Artemis missions to the Moon and on to Mars. This includes sound suppression, fire suppression and cryogenic fluid flow tests, as well as testing the crew access arm and umbilicals — connections that will provide communications, coolant and fuel up until launch.

- While the majority of work for the ground and flight systems is pre-liftoff, the job certainly doesn’t end there.

- “It culminates in a two-day launch countdown in which all of the groups, teams and assets are required to function together in an almost flawless performance to get us to launch,” said Senior NASA Test Director Jeff Spaulding.

- Spaulding has nearly three decades of experience in the Test, Launch and Recovery Office. For Artemis I, he is leading the launch control team and support teams during the launch countdown for Blackwell-Thompson, who will oversee the countdown and liftoff of SLS.

- Just over three miles from the launch pad, on launch day, Spaulding will be in the firing room running the final portion of cryogenic loading through launch. During this time, supercool propellants — called cryogenics — are loaded into the vehicle's tanks. He will perform the same tasks for the wet dress rehearsal, which is a full practice countdown about two months before launch that includes fueling the tanks and replicating everything done for launch prior to main engine start.

- At the end of the mission, part of the team will lead the recovery efforts aboard a Navy vessel after Orion splashdown. The NASA recovery director and supporting NTDs are responsible for planning and carrying out all operations to recover the Orion capsule onto a U.S. Navy ship. This includes working closely with the Department of Defense to ensure that teams coordinate recovery plans, meet requirements, and follow timelines and procedures to bring our heroes and spacecraft home quickly and safely.

- “We are supported by numerous teams at Kennedy and elsewhere around the country that are helping us with our historic first flight as we blaze a path toward landing astronauts on the Moon in 2024,” Spaulding said.

• March 27, 2020: The Orion spacecraft that will fly on the Artemis I mission around the Moon has returned to NASA’s Kennedy Space Center in Florida, USA, after finishing space environment tests. The spacecraft, including ESA’s European Service Module, is now at its final destination before launch. 29) 30)

- Orion spent four months at NASA’s Plum Brook station where it was subjected to the vacuum and temperatures of –175°C to 75°C it will experience on its flight to the Moon. After proving its space-worthiness, the electronics - including the thousands of parameters and functions of the European Service Module that control the engines, electrical power and steering the solar panels to face the Sun - were checked for electromagnetic interference.

- ESA’s Dominique Siruguet from the European Service Module integration and verification team says “The tests were successful and the behavior of the vehicle was good, passing all requirements.”

- Plum Brook station was chosen for the tests because thermal vacuum and electromagnetic compatibility could be performed in the same facility. This avoided additional transport of Orion, which is the size of a two-story house.

- Having passed its trials, the spacecraft was wrapped and moved by truck to an airport in Ohio for its return flight on NASA’s Super Guppy aircraft.

Artemis-I_At Anchor0

Figure 39: Super Guppy leaves Ohio with the Artemis I Orion spacecraft (image credit: NASA, Nicole Smith)

Adding wings to Orion

- The tests are not completely over for Orion, at Kennedy Space Center the crew module will be further prepared and more leak tests conducted. The European Service Module has tanks for fuel, oxygen and water that are critical for the astronauts. The gas tanks are pressurized and are connected to many pipes and valves, so it vital to make sure there are no leaks.

- The solar wings that generate power during its mission will be installed, as well as protective covers called the Spacecraft Adapter Jettisoned fairings for the intense moments of launch on the world’s most powerful rocket.

- Later this year ESA will formally transfer ownership of the European Service Module to NASA and the spacecraft will move into the ground system phase where it will be united with the SLS rocket for a lift-off to the Moon.

- Orion is a key component of Artemis I — an uncrewed test flight around the Moon that paves the way for the Artemis III mission, which will land the first woman and next man on the lunar surface by 2024. ESA is designing and supplying the European Service Module for the Orion spacecraft. This provides electricity, water, oxygen and nitrogen. It also keeps the spacecraft at the right temperature and on course, propelling it to the Moon and back once it has separated from the launcher.

Figure 40: Orion service module – from components to shipping. A look at the elements that make up the European service module that will provide power, water, air and electricity to NASA’s Orion Moon module (video credit: ESA)

March 20, 2020: The following is a statement from NASA Administrator Jim Bridenstine: “NASA leadership is determined to make the health and safety of its workforce its top priority as we navigate the coronavirus (COVID-19) situation. To that end, the agency’s Michoud Assembly Facility and Stennis Space Center are moving to Stage 4 of the NASA Response Framework, effective Friday, March 20. 31)

- “The change at Stennis was made due to the rising number of COVID-19 cases in the community around the center, the number of self-isolation cases within our workforce there, and one confirmed case among our Stennis team. While there are no confirmed cases at Michoud, the facility is moving to Stage 4 due to the rising number of COVID-19 cases in the local area, in accordance with local and federal guidelines.

- “Mandatory telework is in effect for NASA personnel at both facilities until further notice. Additionally, all travel is suspended. These measures are being taken to help slow the transmission of COVID-19 and protect our communities.

- “Access to Stennis and Michoud will be limited to personnel required to maintain the safety and security of the center, as approved by agency leadership and the resident agencies. All previously approved exceptions for onsite work are rescinded and new approvals will be required in order to gain access to the center.

- “NASA will temporarily suspend production and testing of Space Launch System and Orion hardware. The NASA and contractors teams will complete an orderly shutdown that puts all hardware in a safe condition until work can resume. Once this is complete, personnel allowed onsite will be limited to those needed to protect life and critical infrastructure.

- “We realize there will be impacts to NASA missions, but as our teams work to analyze the full picture and reduce risks we understand that our top priority is the health and safety of the NASA workforce.

- “I ask all members of the NASA workforce to stay in close contact with your supervisor and check the NASA People website regularly for updates. Also, in these difficult times, do not hesitate to reach out to the NASA Employee Assistance Program, if needed.

- “I will continue to say, so none of us forget – there is no team better prepared for doing hard things. Take care of yourself, your family, and your NASA team.”

• March 16, 2020: The first Orion spacecraft that will fly around the Moon as part of Artemis to return humans to the lunar surface has finished its space-environment tests at NASA’s Plum Brook Station in Ohio, USA. The vehicle – that can transport up to four astronauts – consists of the European Service Module, the Crew Module and connecting adapter and all elements have now been given the stamp of approval for spaceflight after being subjected to the vacuum, extreme temperatures and electromagnetic interference it will encounter during its trip to the Moon. 32)

- Orion arrived at Plum Brook Station – the only center large enough to test the spacecraft – on 26 November and passed two months of thermal-vacuum tests subjecting the spacecraft to temperatures ranging from –175°C to 75°C in vacuum.

- After passing the trial by temperature, Orion went through electromagnetic interference testing to ensure the electronics worked well together – the European Service Module has over 11 km over wiring to gather information and send commands to its 31 engines, propellant tanks, solar wings and more.

- Orion will now ship to NASA’s Kennedy Space Center where it will be further prepared for launch, including assembling the solar panels and more individual tests.


Figure 41: Orion is a key component of Artemis I, an uncrewed test flight around the Moon that paves the way for the Artemis III mission which will land the first woman and next man on the lunar surface by 2024. ESA is designing and supplying the European Service Module for Orion – the bottom part of the spacecraft in the picture – that provides electricity, water, oxygen and nitrogen as well as keeping the spacecraft at the right temperature and on course (image credit: NASA–Marvin Smith)

• March 3, 2020: Radio frequency testing has begun on the first Orion spacecraft that will fly around the Moon for the Artemis I mission, just two weeks after thermal and environmental tests were completed at NASA’s Plum Brook Station in Ohio, USA. 33)

- EMC (Electromagnetic Compatibility) testing is routine for spacecraft. All electronics emit some form of electromagnetic waves that can cause interference with other devices. Think of the buzz that speakers give out right before an incoming call on a mobile phone.

- Spacecraft electronics can cause similar interference, but out in space such interference can have disastrous consequences, so all systems must be checked before launch.

- EMC tests often take place in a special shielded room constructed of metal walls and doors and foamy spikes (aka Absorbers) that block out unwanted external electromagnetic radiation, like ESA’s Maxwell chamber at its technical site in the Netherlands.

- Though not an EMC chamber, Plum Brook’s thermal vacuum chamber is made of aluminum that does provide electromagnetic shielding, making it a suitable substitute.

- To test electronics, the spacecraft will simulate a flight in realistic conditions with most of its subsystems and equipment powered and in operational mode.

- The electronics are first tested for compatibility in this electromagnetic shielded chamber. Equipment will be switched on to test whether they do potentially disturb one another.

- In the second round of tests, electromagnetic fields will be applied using antennas around the spacecraft to test the susceptibility to interference from external sources. The Orion capsule is equipped with electromagnetic field sensors to take measurements as the disturbance frequencies are injected into the chamber.

- While all subsystems are a potential source of radio frequency noise, of particular interest are the transmitters that intentionally generate radio frequencies. These can easily disturb other equipment sensitive to electromagnetic noise, like GPS receivers, telecommand modules and other communication elements.

- Orion’s European Service Module provides power, propulsion, and crew life support.

- ESA experts are on site monitoring all tests alongside NASA colleagues as Orion moves closer to its first flight without a crew around the Moon.

• January 14, 2020: The first flight of the Artemis program, Artemis I, is scheduled to begin soon. The lunar spacecraft consists of NASA's Orion crew module and the ESM (European Service Module). Developed by ESA and building on technology from its ATV (Automated Transfer Vehicle), the ESM will provide propulsion, life support, environmental control and electrical power to Orion. The Artemis I spacecraft modules are undergoing thermal vacuum and electromagnetic interference tests in the world's largest space simulation vacuum chamber at the Glenn Research Center's Plum Brook Station in Sandusky, Ohio, USA. 34)

Figure 42: Back to the Moon with ESA (video credit: ESA)

• January 13, 2020: NASA’s Kennedy Space Center in Florida will have a busy year preparing facilities, ground support equipment and space hardware for the launch of Artemis I, the first uncrewed launch of the Space Launch System (SLS) rocket and the Orion spacecraft. In 2020, Exploration Ground Systems (EGS) activities will ramp up as launch hardware arrives and teams put systems in place for Artemis I and -2 missions. 35)

Launch Countdown Simulation Activities

Launch countdown simulations will continue to ramp up in 2020 to train and certify the launch control team for Artemis missions. The types of simulations will build on one another and will walk through the final portions of the launch countdown sequence, called the terminal countdown. Integrated simulations will tie in all NASA centers working the mission to ensure all members of the team are ready to work together, including Mission Control at Johnson Space Center in Houston, and the SLS Engineering Support Center at Marshall Space Flight Center in Alabama. Simulations will begin at the end of January and will occur up through one week before launch, with an average of one training exercise each month.

Vehicle Assembly Building

Much of the work in 2020 will be to complete a punch list of detail work inside the VAB (Vehicle Assembly Building). This includes cleaning the platforms and making minor repairs to any platform hardware that will be near flight hardware as the facility prepares for arrival of SLS components and stacking operations.

“We are at a very significant point in NASA’s Artemis mission,” said Mike Bolger, program manager of EGS. “The EGS team has finished mobile launcher testing at the launch pad and will finish testing at the VAB in January. At that point, all of the launch infrastructure will be tested and ready for operations.”

Launch Complex 39B

Teams will continue work on a new emergency egress system for Pad 39B where flight or ground crew could board a basket with a braking system at the crew access level of the mobile launcher. The crew would ride the basket down a cable and come to a stop near a bunker to the west of the pad surface, providing quick escape in the unlikely event of an emergency. The design phase began in 2019 and construction will be complete in time to support crewed Artemis missions.

The pad is currently getting a liquid hydrogen upgrade. The project involves the integration of a new 1.4 million gallon, liquid hydrogen (LH2) storage sphere into the existing Launch Complex 39B system. The new LH2 sphere will work with the current LH2 sphere to supply LH2 for Artemis II and beyond. The larger tank will allow NASA to attempt SLS launches on three consecutive days, instead of opportunities two out of three days, in the event of a scrub. The newer technology reduces liquid hydrogen burn-off, allowing more launch attempts before having to refill the larger tank. Construction began in 2019 and will be complete prior to Artemis II.

Orion Underway Recovery Test 8

The integrated recovery team of NASA, EGS, Lockheed Martin and the U.S. Navy, along with additional contractor support, will head out to sea off the coast of California in March to conduct the eighth Underway Recovery Test. Using a Navy ship with a well deck and several small boats, the primary objective is to validate Orion recovery operations for Artemis I — including procedures and timelines, and practicing different scenarios.

Orion Spacecraft

This spring, the Orion spacecraft for Artemis I will return from NASA’s unique test facility at Plum Brook Station in Ohio, where it is currently undergoing environmental testing inside the vacuum chamber that simulates the harsh environment of space. Inside the Neil Armstrong Operations and Checkout (O&C) Building at Kennedy, technicians will install the spacecraft’s solar array wings before performing final checkouts. EGS will begin Orion ground processing and stacking activities later in the year. The team will process and fuel Orion in the Multi-Purpose Processing Facility then transfer it over to the Launch Abort System Facility where engineers will attach the launch abort system. Orion will then roll out to the VAB for inspections before stacking Orion on top of the SLS rocket.

In its early processing stages, the Artemis II crew module milestones inside the O&C include propulsion tank installation, a pressure test and subsystems installations in the spring. The initial power-on of the crew module will occur in early fall. The heat shield that will protect the first crewed mission of Orion will be completed and installed by the end of the year. Processing and testing of the crew module adapter – the ring that connects to the European Service Module – for Artemis II will happen in the first half of the year prior to the arrival of the European Service Module in the fall.

SLS (Space Launch System)

Training activities with pathfinders, or full-scale replicas, of the SLS core stage and booster segments occurred in 2019, and more training with various pathfinder segments and hardware will continue. In 2020, training will involve stacking inert booster segments on the mobile launcher in the VAB.

Hardware for SLS will continue to arrive for processing and integration in various Kennedy facilities. This year all ten of the solid propellant booster segments will arrive by train from their Northrop Grumman manufacturing facility in Promontory, Utah. The launch vehicle stage adapter, which will connect the SLS core stage to the interim cryogenic propulsion stage, will arrive by barge. The booster aft skirts – which contain the thrust vector control system that steers the rocket – will trek from the Booster Fabrication Facility to the Rotation, Processing and Surge Facility where they will be attached to the aft exit cones. The exit cones are attached to the bottommost part of each of the twin boosters to provide extra thrust to the boosters and protect the aft skirts from the thermal environment during launch.

The core stage of the SLS rocket will undergo a Green Run test campaign over several months in the B-2 test stand at the agency’s Stennis Space Center in Mississippi. Following Green Run completion, the 225,000-pound core stage will leave Stennis and arrive at Kennedy on the Pegasus barge. The core stage and solid rocket boosters will then be integrated inside the VAB.

Mobile Launcher 2

In 2019, NASA awarded a contract for Mobile Launcher 2 to Bechtel National Inc. of Reston, Virginia. The ground structure that will be used to assemble, process and launch the second and more powerful configuration of the SLS rocket, called Block 1B, is in its early stages of design and development and will be ready for Artemis-4.

Artemis I will be the first in a series of increasingly challenging missions that will enable human exploration to the Moon and Mars. In 2020, the mission will truly begin to take shape as hardware arrives and stacking operations begin inside the VAB.

“The operations team is writing procedures, training, and preparing for flight hardware processing,” Bolger said. “When the SLS and Orion are turned over to EGS later this year, Kennedy will be ready!”

Future Artemis missions will establish a sustainable presence at the Moon for decades to come, and Kennedy teams will move forward in 2020 to build the infrastructure and make those missions possible.

• December 17, 2019: Europe will power the NASA spacecraft that take astronauts to a new international outpost and forward to the Moon, following decisions made by ESA Member States at Space19+ in Seville, Spain. 36)

- The decision by Member States show a strong commitment to progressing Europe’s exploration of the Solar System and will see ESA play a key role in Artemis missions by providing European Service Modules for Orion spacecraft three and four.

- The Orion spacecraft is built by NASA with ESA providing the service module. The arrangement stems from the international partnership for the International Space Station. NASA’s decision to cooperate with ESA on a critical element for the mission is a strong sign of trust and confidence in ESA’s capabilities.

- More than 20 companies around Europe are now building the European Service Module as NASA works on Orion and the Space Launch System.

- ESA is already providing the European Service Modules that will power missions one and two. The first Artemis mission will see Orion fly without astronauts around the Moon, with the second mission flying with astronauts on a direct return trajectory around the Moon.

- Under current Artemis planning, the third and fourth missions will see NASA’s Orion spacecraft bring astronauts to the Gateway and on to a landing on the lunar surface.

- The news confirms that humankind’s return to the Moon will be truly international, strengthening the collaboration between NASA and ESA on Orion, Artemis and much more.

- Space19+ results also give ESA mandate to start procuring ‘long-lead items’ that require more time to develop and build – allowing industrial partners to prepare early equipment needed for a fifth and sixth European Service Module.

- The first European Service Module is currently at NASA’s Plum Brook Station in Ohio, USA, coupled to the Crew Module and Service Module Adapter for thermal-vacuum and electromagnetic tests on the complete Orion spacecraft.

- The second European Service Module is being built in Bremen, Germany, by prime contractor Airbus. The structure is complete and technicians are working round the clock to complete the module, starting with integration of 11 km of wiring.

- NASA is committed to landing on the Moon by 2024 and Europe is now a trusted lunar partner, supplying the modules to propel Orion and support the astronauts with energy and consumables en route.


Figure 43: Exploration Mission-1 step-by-step. Orion is NASA’s next spacecraft to send humans into space. It is designed to send astronauts farther into space than ever before, beyond the Moon to asteroids and even Mars. ESA has designed and is overseeing the development of Orion’s service module, the part of the spacecraft that supplies air, electricity and propulsion. Much like a train engine pulls passenger carriages and supplies power, the European Service Module will take the Orion capsule to its destination and back (image credit: ESA–K. Oldenburg)

• December 4, 2019: Here at NASA’s Plum Brook Station in Ohio, USA, Orion is being put into a thermal cage in preparation of getting its first feel of space in the world’s largest thermal vacuum chamber. 37)


Figure 44: The Orion spacecraft with European Service Module at NASA’s Plum Brook Station. The first Orion will fly farther from Earth on the Artemis I mission than any human-rated vehicle has ever flown before – but first it will undergo testing to ensure the spacecraft withstands the extremes of spaceflight. In this figure, Orion is being placed in a cage, called the Thermal Enclosure Structure (TES), that will radiate infrared heat during the tests inside the vacuum chamber (image credit: ESA, S. Corvaja)

- Orion will be subjected to temperatures at Plum Brook ranging from –115°C to 75°C in vacuum for over two months non-stop – the same temperatures it will experience in direct sunlight or in the shadow of Earth or the Moon while flying in space.

- The tests that will be run over the next few months will show that the spacecraft works as planned and adheres to the strictest safety regulations for human spaceflight. The European Service Module has 33 thrusters, 11 km of electrical wiring, four propellant and two pressurization tanks that all work together to supply propulsion and everything needed to keep astronauts alive far from Earth – there is no room for error.

• November 27, 2019: Plum Brook Station is a remote test facility for the NASA Glenn Research Center in Cleveland, Ohio. Plum Brook is home to the world’s largest and most powerful space environment simulation facilities including the Space Simulation Vacuum Chamber. 38)


Figure 45: The Reverberant Acoustic Test Facility is the world's most powerful spacecraft acoustic test chamber, which can simulate the noise of a spacecraft launch up to 163 decibels or as loud as the thrust of 20 jet engines. The Mechanical Vibration Facility is the world's highest capacity and most powerful spacecraft shaker system, subjecting test articles to the rigorous conditions of launch. The Orion spacecraft and its European Service Module is tested here to ensure it will withstand the extremes of spaceflight (image credit: NASA)

• November 26, 2019: The Artemis I Orion spacecraft arrived at NASA’s Plum Brook Station in Sandusky, Ohio, on Tuesday, Nov. 26 for in-space environmental testing in preparation for Artemis I. 39) 40)


Figure 46: The Orion spacecraft being lifted onto the truck for transport to NASA's Plum Brook Station (image credit: NASA)

- This four-month test campaign will subject the spacecraft, consisting of its crew module and European-built service module, to the vacuum, extreme temperatures and electromagnetic environment it will experience during the three-week journey around the Moon and back. The goal of testing is to confirm the spacecraft’s components and systems work properly under in-space conditions, while gathering data to ensure the spacecraft is fit for all subsequent Artemis missions to the Moon and beyond.

- “This is the final critical step before the spacecraft is ready to be joined with the Space Launch System rocket for this first test flight in 2020,” said Dr. Marla Pérez-Davis, acting director, NASA’s Glenn Research Center. “Our team at Plum Brook Station has been upgrading the Space Environments Complex to prepare for this test, and we are thrilled that it is here.”

- The spacecraft flew into Mansfield Lahm Airport aboard the agency’s Super Guppy from NASA’s Kennedy Space Center in Florida, where engineers and technicians recently completed assembly and integration of the crew capsule and service module. Transportation of the spacecraft is an involved process, bringing together teams from Glenn, Kennedy, NASA’s Johnson Space Center in Houston, Lockheed Martin, the Ohio Air National Guard, and the following local logistics companies: RPTS Express; Diamond Heavy Haul, Inc.; and Capital City Group, Inc.

- “This is an exciting day for our state, as it continues Ohio’s long line of history in our nation’s space exploration pursuits,” said U.S. Rep. Troy Balderson. “From the Wright brothers to the first man on the Moon—Neil Armstrong—to the Orion spacecraft, Ohio leads the United States in the aerospace industry and will continue to do so in the future.”

- After unloading Orion at the airport, the transportation team drove the spacecraft across Northeast Ohio’s new space corridor. NASA Glenn worked with the Ohio Department of Transportation and local utility companies to clear more than 700 overhead lines from the 41-mile stretch of rural highway between Mansfield and Plum Brook Station. The space corridor creates new opportunities for Ohio by enabling Plum Brook to conduct large-scale testing of agency and commercial spacecraft previously unachievable due to logistics challenges.

- “This next-generation Orion spacecraft is being tested at NASA Plum Brook because of our region’s world-class workforce and unrivaled experience in space exploration,” said U.S. Rep. Marcy Kaptur. “NASA Plum Brook has a long and storied history at the center of America’s leadership in space exploration. Congratulations to the scientists, engineers and technicians for the hard work that it took get us to this point. Today’s arrival culminates years of planning, coordination and construction. This momentous occasion is an important step on the path to a future manned mission to the Moon.”

- Artemis I is an uncrewed test flight around the Moon, the first in a series of progressively more complex missions that will land the first woman and next man on the lunar surface by 2024. NASA will then use what it learns on the Moon to prepare to send humans to Mars.

• November 22, 2019: The Orion crew and service module stack for Artemis I was lifted out of the Final Assembly and Test (FAST) cell on Monday, November 11. The spacecraft has been stationed in the FAST cell since July 2019 for mating and closeout processing. 41)

- After lifting out of the cell, Orion will be attached to a tool called a verticator that rotates the stack from its vertical configuration to a horizontal configuration for transport to NASA’s Plum Brook Station in Sandusky, Ohio, USA, where it will undergo full environmental testing to certify the complete vehicle for flight.

- Once the vehicle returns to NASA's Kennedy Space Center it will return to the FAST cell for installation of final panels left off for environmental testing purposes and the service module’s four solar arrays.


Figure 47: The service module and crew module were moved separately into the cell, stacked and connected together for the mission (image credit: NASA, Rad Sinyak)

• October 23, 2019: ESA and NASA reaffirmed their interest in working with commercial service providers as well as international partners on missions to the Moon in a joint statement signed at the 70th annual International Astronautical Congress last week. 42)

- The statement supports the ‘Lunar Pathfinder’ mission, ESA’s first Moon partnership with European industry, addressing communication and navigation needs for future lunar exploration.

- The ‘Lunar Pathfinder’ partnership helps lay the foundation for providing communications, navigation, and operations services around the Moon. Its communications relay service is intended to link the Earth and the lunar surface.

- “We are working together to make the commercial lunar economy a reality,” says David Parker ESA’s Director of Human and Robotic Exploration. “We want to act as an anchor customer and institutional broker for gaining access to non-European markets. ESA supports a competitive ecosystem of European space providers.”

- Commercialization is gaining momentum in the space arena and both ESA and NASA confirmed their intention to work on lunar services with the UK Space Agency earlier this year.

- The move follows ESA’s collaboration agreement with UK partners Surrey Satellite Technology Ltd and Goonhilly Earth Station for support in lunar services, signed in April 2018.

- In the joint statement, NASA and ESA reiterated their interest to identify the elements of this potential cooperation and formalize an interagency agreement in the future.

- The two agencies have also committed to working together to supplement NASA’s own communications capabilities with those of ESA and its partners.

- NASA also confirmed its interest in having a variety of communication and navigation services to serve its robotic missions, including lunar surface activities, starting as early as end of 2022.


Figure 48: David Parker ESA’s Director of Human and Robotic Exploration and Thomas Zurbuchen NASA's Associate Administrator for Science signed a joint statement that welcomed the ‘Lunar Pathfinder’ mission, ESA’s first Moon partnership, during the 70th annual International Astronautical Congress. Alice Bunn, director of International Policy at the UK Space Agency, and Sir Martin Sweeting, founder and executive chairman of Surrey Satellite Technology Ltd. (SSTL), were also present during the signature (image credit: ESA)

• July 20, 2019: The goal of humans again walking on the Moon is one giant leap closer. Lockheed Martin has completed building the capsule for NASA's Orion spacecraft. The crew module capsule for the uncrewed Artemis 1 mission to the Moon has been stacked on top of the Orion service module, which was also recently finished. 43)

- Vice President Mike Pence made the announcement today at a ceremony in front of the Orion spacecraft in the aptly-named Neil Armstrong Operations and Checkout Building at the Kennedy Space Center in Florida. The event and announcement commemorated the 50-year anniversary of the Apollo 11 Moon landing.

- The Orion spacecraft is like none other in its design and capability.

- "Orion is a new class of spaceship, uniquely designed for long-duration deep space flight, that will return astronauts to the Moon and eventually take the first humans to Mars, and bring them all back safely." said Lisa Callahan, vice president and general manager of Commercial Civil Space at Lockheed Martin. "Orion will accelerate scientific discovery of our solar system and will be the cornerstone of the defining space achievement of this era."

- Since the crew module pressure vessel arrived in Florida, technicians and engineers from Lockheed Martin, NASA and supporting contractors have meticulously assembled the capsule into its finished state. The work included installing the capsule's avionic computers, harnesses, propulsion system and its 12 engines, 11 parachutes, its large 16-foot-diameter heat shield, forward bay cover and numerous other systems and components.

- Throughout assembly, the team tested and validated the many systems a hundred different ways to ensure they will operate as designed in the harshness of deep space," said Mike Hawes, Orion program manager for Lockheed Martin. "The Artemis 1 flight will test the design and workmanship of the capsule and its service module during the three-week mission out around the Moon and back. We're excited for this mission as it paves the way for the first crewed mission in 2022, Artemis 2."

- The crew module and service module were stacked together earlier in the week in the Final Assembly and System Testing (FAST) cell where they are now being fully integrated, including connecting the physical retention bolts and the umbilical lines between the two modules. The FAST cell is also where the Apollo spacecraft were integrated.

- The combined stack will then be powered up and undergo a series of integrated systems tests. In September, the combined stack will be shipped to NASA's Plum Brook Station in Ohio, where it will go through environmental testing in a large thermal vacuum chamber as well as testing for electromagnetic interference and compatibility.

- Once Orion returns to Kennedy at the end of the year, the spacecraft will go through final preparations before Lockheed Martin delivers it to ground systems for launch processing in early 2020.


Figure 49: On the 50th anniversary of the Apollo Moon landing, the Lockheed Martin-built Orion capsule for the Artemis 1 mission to the Moon is declared finished (image credit: Lockheed Martin)

• July 02, 2019: NASA successfully demonstrated on Tuesday the Orion spacecraft’s launch abort system can outrun a speeding rocket and pull astronauts to safety during an emergency during launch. The test is another milestone in the agency’s preparation for Artemis missions to the Moon that will lead to astronaut missions to Mars. 44)

- During the approximately three-minute test, called Ascent Abort-2, a test version of the Orion crew module launched at 7 a.m. EDT from Space Launch Complex 46 at Cape Canaveral Air Force Station in Florida on a modified Peacekeeper missile procured through the U.S. Air Force and built by Northrop Grumman.

- The Orion test spacecraft traveled to an altitude of about six miles, at which point it experienced high-stress aerodynamic conditions expected during ascent. The abort sequence triggered and, within milliseconds, the abort motor fired to pull the crew module away from the rocket. Its attitude control motor flipped the capsule end-over-end to properly orient it, and then the jettison motor fired, releasing the crew module for splashdown in the Atlantic Ocean.

Figure 50: A fully functional Launch Abort System (LAS) with a test version of the Orion spacecraft attached, launches on NASA’s Ascent Abort-2 (AA-2) atop a Northrop Grumman provided booster on July 2, 2019, at 7 a.m. EDT, from Launch Pad 46 at Cape Canaveral Air Force Station in Florida. During AA-2, the booster will send the LAS and Orion to an altitude of 31,000 feet at Mach 1.15 (more than 1,000 mph). The flight test will prove that the abort system can pull crew to safety in the unlikely event of an emergency during ascent (video credit: NASA Kennedy, Published on 2 July 2019)

- A team is collecting the 12 data recorders that were ejected during the test capsule’s descent. Analysis of the information will provide insight into the abort system’s performance.

- “We're building the most powerful rocket in the world to send astronauts to the Moon in the Orion spacecraft for Artemis missions,” said Bill Hill, deputy associate administrator for Exploration Systems Development at NASA Headquarters in Washington. “With this exploration system designed to safely carry humans farther into space than ever before, we'll also have an equally powerful launch abort system that will pull the crew away if there is a problem with the rocket during the early portion of ascent.”

- The tower-like abort structure consists of two parts: the fairing assembly, which is a shell composed of a lightweight composite material that protects the capsule from the heat, air flow and acoustics of the launch, ascent, and abort environments; and the launch abort tower, which includes the abort motor, attitude control motor, and jettison motor. The system is built specifically for deep space missions and to ride on NASA’s powerful Space Launch System (SLS) rocket.

- “Launching into space is one of the most difficult and dangerous parts of going to the Moon,” said Mark Kirasich, Orion program manager at Johnson Space Center in Houston. “This test mimicked some of the most challenging conditions Orion will ever face should an emergency develop during the ascent phase of flight. Today, the team demonstrated our abort capabilities under these demanding conditions and put us one huge step closer to the first Artemis flight carrying people to the Moon.”

- NASA was able to accelerate the test schedule and lower costs by simplifying the test spacecraft and eliminating parachutes and related systems. NASA already qualified the parachute system for crewed flights through an extensive series of 17 developmental tests and eight qualification tests completed at the end of 2018.

- Engineers are making progress building and testing the Orion spacecraft for Artemis 1, the first uncrewed mission with the SLS rocket – an integrated system traveling thousands of miles beyond the Moon – and for Artemis 2, the first mission with astronauts.

- At NASA’s Kennedy Space Center in Florida, technicians are preparing to attach the Orion crew and service modules before testing at the agency’s Plum Brook Station in Sandusky, Ohio, later this year. The crew module for Artemis 2 is being outfitted with thousands of elements – from bolts and strain gauges to parachutes and propulsion lines.

- The agency recently reached major milestones for the SLS rocket, assembling four of the five parts that make up the massive core stage that will launch Artemis 1 and delivering the four engines that will be integrated into the core stage, along with the engine section, later this summer. When completed, the entire core stage will be the largest rocket stage NASA has built since manufacturing the Saturn V stages for NASA’s Apollo lunar missions in the 1960s.

- Orion is part of NASA’s backbone for deep space exploration, along with the SLS and Gateway, that will land the first woman and next man on the Moon by 2024. Through the Artemis program, the next American Moon walkers will depart Earth aboard Orion and begin a new era of exploration.

• March 28, 2019: ESA Director of Human and Robotic Exploration, David Parker, and Associate Administrator for NASA’s Science Mission Directorate, Thomas Zurbuchen, signed a Statement of Intent to coordinate joint science research about the Moon and identify opportunities for lunar mission cooperation. 45)

- Signed during the National Academies’ Space Science Week in Washington DC, the statement highlights a common interest in accessing the Moon, driven by scientific discovery and support for private-sector capabilities, and mission services on the lunar surface and in the vicinity of the Moon.

- “We are thrilled to be bringing European expertise to the table,” said David, “and to work collaboratively to prepare the way to a sustainable presence on the Moon where nations and the private sector work together to deliver benefits for all the people of Earth.”

Soon to the Moon

- The Moon has once again captured the attention of space agencies as an 'archive' of cosmic history and a cornerstone for planetary science. Water ice and other possible resources at the Moon offer the possibility of the Moon becoming a 'stepping stone' to the wider Solar System. The US Vice President Mike Pence directed NASA on March 26 to accelerate a human return to the Moon in the next five years.

- ESA’s proposal to its Member States for the next period of its European Exploration Program includes continuing its involvement in endeavors in low Earth orbit as well as around and on the Moon and Mars. This will allow scientific research, development of key technologies and international cooperation – inspiring missions that expand humankind's presence beyond Earth.

- In going forward to the Moon, ESA and NASA are committed to sustainable lunar exploration made possible by cooperation – not only with space agencies but also with the private sector. New commercial capabilities offer new opportunities to explore – and to expand economic activity into deep space. Both agencies will continue to explore scientific collaboration on payloads and future missions to the Moon.

- Teaming up is nothing new for ESA and NASA, with both agencies working together on the International Space Station, robotic missions and more recently on the Orion spacecraft, the first spacecraft capable of delivering a crew to the Moon since 50 years.

- ESA is supplying the European Service Module for Orion, in an arrangement that stems from the International Space Station partnership. Based on ESA’s proven Automated Transfer Vehicles for supplying the International Space Station, the module will provide everything to keep the astronauts alive, including oxygen, water, thermal control, electricity and propulsion.

- ESA looks forward in cooperation and collaboration to probe the mysteries of the Moon and to use insights found as a springboard towards humankind’s future in deep space.


Figure 51: Thomas Zurbuchen, NASA’s Associate Administrator for the Science Mission Directorate (left), and David Parker, ESA’s Director of Human and Robotic Exploration, signing a Statement of Intent to coordinate joint science research about the Moon and identify cooperative lunar mission opportunities during the National Academies’ Space Science Week in Washington, DC, USA, on 27 March 2019. The statement highlights a common interest in accessing the Moon driven by scientific discovery and support for private-sector capabilities and mission services on the surface and in the vicinity of the Moon (image credit: ESA, M. Tabache)

November 7, 2018: European module arrives at Kennedy Space Center: After a 24-hour journey from Bremen, Germany with stops in Hamburg and Portsmouth, USA, the European Service Module landed yesterday at Kennedy Space Center in Florida. The Antonov An-124 aircraft landed on 6 November 2018 at 11:35 EST, local time. 46)

- The first service module is a key component that will see Orion around the Moon for Exploration Mission-1. It will make the powerful burns required to enter and exit lunar orbit as well as softer burns to allow for space maneuvering and course correction. After years of designing, building, and testing in Europe, the powerhouse that will propel NASA’s Orion spacecraft to the Moon will soon be mated with the rest of the spacecraft to undergo final testing before flight.

- The European Service Module is a truly European endeavor. Primary components were built and integrated in Italy and Germany, with smaller components delivered from several European nations, including the solar arrays from the Netherlands.

- ESA’s partnership with NASA takes this European effort to the global stage. For the first time, NASA will use a European-built system as a critical element to power an American spacecraft, extending the international cooperation of the International Space Station into deep space.

- The trust in European know-how is thanks to the successful Automated Transfer Vehicle (ATV) program that provided reliable cargo deliveries to the Space Station. ATV’s engineering and operational legacy were crucial to developing the European Service Module, which some of its flight-proven hardware, such as the auxiliary thrusters and pressurization tanks.


Figure 52: Orion: an international collaboration. Orion is NASA’s next spacecraft to send humans into space. It is designed to send astronauts farther into space than ever before, beyond the Moon to asteroids and even Mars. ESA has designed and is overseeing the development of Orion’s service module, the part of the spacecraft that supplies air, electricity and propulsion. Much like a train engine pulls passenger carriages and supplies power, the European Service Module will take the Orion capsule to its destination and back (image credit: ESA, K. Oldenburg)

Legend to Figure 52: The Orion spacecraft is built by NASA with ESA providing the service module. The arrangement stems from the international partnership for the International Space Station. NASA’s decision to cooperate with ESA on a critical element for the mission is a strong sign of trust and confidence in ESA’s capabilities. More than 20 companies around Europe are now building the European Service Module as NASA works on Orion and the Space Launch System.

- Next steps: Next up for the ESM-1 (European Service Module-1) is unloading and unpacking. The unit will be checked for integrity after its transatlantic flight and then unloaded in the Operations & Checkout (O&C) building at Kennedy Space Center.

- Some parts of the ESM-1 have already been shipped by sea in two containers and are already awaiting the arrival of the larger air shipment. These include nozzle covers, heat shield, and insulation layers, among other components. The solar arrays will arrive in February 2019.

- Once in the O&C, the ESM-1 will be fitted to the Crew Module Adapter (CMA) to form the Orion Service Module. This process takes some time, as all fluid and gas pipes must be welded and electrical wiring connected. The crew module will then be mated with the service module and the completely integrated spacecraft will head to NASA Glenn Research Center’s Plum Brook Station in Ohio for a 60-day test campaign. The entire spacecraft will be subjected to intense launch conditions in the world’s largest vacuum chamber.

- Once complete, the spacecraft will travel back to Kennedy Space Center to meet its launcher, the Space Launch Systems (SLS) rocket, and prepare for its first mission, a lunar orbital mission without astronauts, to demonstrate the spacecraft’s capabilities.

- Work is already underway on the second European Service Module which will provide air, water, and temperature control for the astronauts that will fly on Orion’s Exploration Mission-2.

- ESA is immensely proud to play a crucial role in humanity’s return to the Moon, thanks to the hard work and determination of the many teams involved in bringing the European Service Module to this next step on the journey back to the Moon.

November 6, 2018: The powerhouse that will help NASA’s Orion spacecraft venture beyond the Moon is stateside. The European-built service module that will propel, power and cool during Orion flight to the Moon on Exploration Mission-1 arrived from Germany at the agency’s Kennedy Space Center in Florida on Tuesday to begin final outfitting, integration and testing with the crew module and other Orion elements (Figure 53). 47)

- The service module is integral to human missions to the Moon and Mars. After Orion launches on top of the agency’s Space Launch System rocket, the service module will be responsible for in-space maneuvering throughout the mission, including course corrections. The service module will also provide the powerful burns to insert Orion into lunar orbit and again to get out of lunar orbit and return to Earth. It is provided by ESA (European Space Agency) and built by ESA’s prime contractor Airbus of Bremen, Germany. NASA’s prime contractor for Orion, Lockheed Martin, built the crew module and other elements of the spacecraft.

- “We have a strong foundation of cooperation with ESA through the International Space Station partnership, and the arrival of the service module signifies that our international collaboration extends to our deep space human exploration efforts as well,” said Bill Gerstenmaier, NASA’s associate administrator for Human Exploration and Operations.

- The European-built service module brings together new technology and lightweight materials while taking advantage of spaceflight-proven hardware. It is comprised of more than 20,000 components, including four solar array wings that provide enough electricity to power two three-bedroom homes, as well as an orbital maneuvering system engine, a recently refurbished engine previously used for in-orbit control by the space shuttle. Beginning with Exploration Mission-2, the module also will provide air and water for astronauts flying inside Orion, which will carry people to destinations farther than anyone has travelled before and return them safely to Earth.

- “Our teams have worked together incredibly hard to develop a service module that will make missions to the Moon and beyond a reality,” said Mark Kirasich, NASA’s Orion program manager. “It is quite an accomplishment of ESA and Airbus to have completed the developmental work on the module and have this major delivery milestone behind us.”

- Now that the service module is at Kennedy, it will undergo a host of tests and integration work ahead of Exploration Mission-1. Engineers will complete functional checkouts to ensure all elements are working properly before it is connected to the Orion crew module. Teams will weld together fluid lines to route gases and fuel and make electrical wiring connections. The service module and crew module will be mated, and the combined spacecraft will be sent to NASA’s Glenn Research Center’s Plum Brook Station in Ohio early next year where it will undergo 60 days of continuous testing in the world’s largest thermal vacuum chamber to ensure Orion can withstand the harsh environment of deep space. Once that testing is complete, it will return to Kennedy for integration with the SLS rocket in preparation for launch.

- NASA is leading the next steps to establish a permanent human presence at the Moon. The first in a series of increasingly complex missions, Exploration Mission-1 is a flight test of an uncrewed Orion spacecraft and SLS rocket that will launch from NASA’s modernized spaceport at Kennedy. The mission will send Orion 40,000 miles beyond the Moon and back and pave the road for future missions with astronauts. Together, NASA and its partners will build the infrastructure needed to explore the Moon for decades to come while laying the groundwork for future missions to Mars.


Figure 53: The European Service Module for NASA's Orion spacecraft was loaded on an Antonov airplane in Bremen, Germany, on Nov. 5, 2018, for transport to NASA's Kennedy Space Center in Florida. For the first time, NASA will use a European-built system as a critical element to power an American spacecraft, extending the international cooperation of the International Space Station into deep space (image credit: NASA/Rad Sinyak)

• October 30, 2018: The European Service Module that will power and propel the Orion spacecraft on its first mission around the Moon will ship early next week from Bremen to the United States. It will take off in an Antonov An-124 aircraft in the early hours of 5 November and arrive at Kennedy Space Center in Florida, US on 6 November. 48)

- Designed and manufactured in Italy and Germany, the powerful workhorse is Europe’s contribution to humanity’s return to the Moon.

- Trusted partner: For the first time, NASA will use a European-built system as a critical element to power an American spacecraft, thanks in large part to ESA’s successful Automated Transfer Vehicle (ATV) program that brought supplies to the International Space Station.

- The knowledge gained by ESA and European industry from designing, building and operating the complex and successful Automated Transfer Vehicle missions was instrumental for ESA’s participation in NASA’s Orion spacecraft.

- The unit resembles ATV, from which it evolved. Three types of engine will propel Orion to its destination and can turn it in all directions to align the spacecraft as needed.

- Inside the European Service Module, large tanks hold fuel as well consumables for the astronauts: oxygen, nitrogen and water.

- Radiators and heat exchangers keep the astronauts and equipment at a comfortable temperature, while the module’s structure is the backbone of the entire vehicle, like a car chassis.

- The European Service Module was built by main contractor Airbus Defence and Space, with many companies all over Europe supplying components.

- Once at Kennedy Space Center, the European Service Module will be connected to the Orion crew module and its adapter in preparation for Exploration Mission-1 – a test flight without astronauts that will travel farther into space than any human-rated spacecraft has ventured. The mission is expected to launch in 2020.

- Work is already underway on the second European Service Module that will power a crewed mission around the Moon.

- The Orion spacecraft will eventually launch together with components of the Gateway, a human-tended outpost in lunar orbit that will aid human and robotic exploration of the Moon.

• October 29, 2018: Aerojet Rocketdyne recently completed qualification testing for the enhanced reaction control thruster system for NASA’s Orion crew vehicle, helping to clear the way for the Lockheed Martin-built spacecraft’s second test flight, and first mission to cislunar space, called Exploration Mission-1 (EM-1). 49)

- The RCS (Reaction Control System) is the only means of guiding the Orion crew module after it separates from its service module in preparation for atmospheric reentry and subsequent splashdown. Consisting of 12 MR-104G hydrazine thrusters capable of 160 pounds of thrust each, the system also will ensure that the spacecraft is properly oriented (with its heat shield pointed downward) for reentry, and stable during descent.

- Aerojet Rocketdyne employed cutting-edge additive manufacturing processes, also known as 3D printing, in fabricating the RCS engine nozzle extensions. These 3D printed components, along with other items on the spacecraft, mark one of the first times in history that a spacecraft carrying humans will incorporate additively manufactured parts.

- “Additive manufacturing eliminates traditional design constraints, as well as reduces manufacturing times,” said Eileen Drake, Aerojet Rocketdyne CEO and president. “Our use of 3D printing on Orion is just one example of how we are incorporating this breakthrough technology across our portfolio of propulsion products.”

- During the yearlong qualification test program at Aerojet Rocketdyne’s Redmond, Washington, facility, a single engine was subjected to shock and vibration, exceeding the maximum stresses expected during the upcoming EM-1 launch. For EM-1, Orion will be launched toward the Moon on the maiden flight of NASA’s Space Launch System (SLS) rocket. The non-flight test engine – drawn from the same production lot as the EM-1 RCS flight engines – burned through 619 pounds of propellant during the test program, accumulating 962 seconds of total firing time.

- “Following our rigorous qualification testing program, we’re confident that this enhanced RCS system is ready to fly,” added Drake. “The reaction control thrusters are critical to the Orion capsule’s safe return to Earth at the completion of EM-1 as well as future crewed missions.”

- The EM-1 RCS thruster design builds on the flight proven engine demonstrated on the Exploration Flight Test-1 mission in 2014. The enhanced system features a stronger structure, increased resistance to thermal stresses and reduced mass. The improved manufacturing process updated the system to account for changed loads and to ultimately increase affordability.

- On EM-1 an uncrewed Orion spacecraft will launch into a distant retrograde orbit around the Moon before returning to Earth for a splashdown in the Pacific Ocean. It will be followed by EM-2, during which Orion will fly near the Moon with astronauts on board.

- In addition to the RCS, Aerojet Rocketdyne is supplying the main- and upper-stage liquid engines for the SLS, and well as the jettison motor that will separate Orion’s launch abort system from the crew module shortly after activation of the SLS’s second stage. The company also is supplying the auxiliary thrusters for Orion’s European Service Module (ESM), and supported a NASA-led effort to modify a Space Shuttle OMS-E engine, originally built by Aerojet Rocketdyne for its new application as the ESM main maneuvering engine.

• October 23, 2018: After years of planning, development, building and integration, the European Service module that will power the Orion spacecraft on its journey into lunar space is ready to be shipped. In November the fully integrated, tested, and sealed European workhorse will leave Bremen on an Antonov cargo plane for Kennedy Space Center in Florida, USA where it will be integrated with the rest of the Orion spacecraft. 50)

- ESA’s European service module will provide power, water, air and electricity to NASA’s Orion exploration spacecraft that will eventually fly beyond the Moon with astronauts. The European Service Module is now complete for Orion’s first mission that will do a lunar fly-by without astronauts to demonstrate the spacecraft’s capabilities.

- Orion’s solar wings will be shipped separately, also from Bremen. In the USA the module will be stacked together with NASA’s Crew Module Adaptor and Crew Module, the first time the complete spacecraft will be on display.

- More tests await the Orion spacecraft at NASA’s Plum Brook facility where it will be put in the world’s largest vacuum chamber to simulate spaceflight as well as being subjected to acoustic tests to simulate the intense vibrations Orion will endure when launched on the world’s largest rocket, NASA’s Space Launch Systems.

- This is a proud moment for Europe. For the first time, NASA will use a European-built system as a critical element to power an American spacecraft, extending the international cooperation of the International Space Station into deep space.

- Work is already underway on the second European Service Module. The structure is complete and over 11 km of cables are being meticulously placed in preparation for the computers and equipment that will keep astronauts alive and well for the second Orion mission called EM-2 (Exploration Mission-2).


Figure 54: Human and robotic exploration image of the week: The European Service Module of the Orion spacecraft is ready for shipment to the US (image credit: Airbus)

• October 2018: Following a very successful year of manufacturing, assembly and testing in factories located around the globe, NASA and ESA are preparing to deliver the major Exploration Mission-1 (EM-1) Orion flight elements, including the Crew Module, ESA Service Module and Launch Abort System. This international effort to design and develop a deep space exploration capable human spacecraft is rapidly transitioning from the design, development and test phase to the early test flight and production phase. Two major flight tests, an Ascent Abort test and EM-1, Orion's first flight onboard NASA's new heavy lift Space Launch System, are planned for the near future. Further, Orion will play a crucial role in the ambitious new Deep Space Gateway human exploration Program. 51)

• September 18, 2018: Last week at the Airbus integration hall in Bremen, Germany, technicians installed the last radiator on the European Service Module for NASA’s Orion spacecraft marking the module’s finished integration. 52)

- ESA’s European service module will provide power, water, air and electricity to NASA’s Orion exploration spacecraft that will eventually fly beyond the Moon with astronauts. The European Service Module is now complete for Orion’s first mission that will do a lunar fly-by without astronauts to demonstrate the spacecraft’s capabilities.


Figure 55: Technicians instal the radiators on the European Service Module for NASA’s Orion spacecraft marking the module’s finished integration (image credit: ESA–A. Conigli)

- Much like closing the bonnet on a car, with the radiators in place technicians can no longer access the internals of the European service module, symbolically ending the assembly and integration of the module that will fly further into our Solar System than any other human-rated spacecraft has ever flown before.

- Technicians worked 24 hours a day in three shifts to complete the service module’s assembly which is now going through the last stages of its extensive testing. Engineers will put the module through its paces with functional tests that include checking the newly installed radiators and testing the propulsion system with its intricate pipelines that deliver fuel and oxidizer to the spacecraft’s 33 engines.


Figure 56: View from below: Orion European Service Module-1. Technicians work underneath the European Service Module for NASA’s Orion spacecraft, September 2018 (image credit: ESA–A. Conigli)

- Once complete the service module will be packed and flown to NASA’s Kennedy Space Center in Florida, USA. Orion’s solar wings will be shipped separately, also from Bremen. In the USA the module will be stacked together with NASA’s Crew Module Adaptor and Crew Module, the first time the complete spacecraft will be on display.

- More tests await the Orion spacecraft at NASA’s Plum Brook facility where it will be put in the world’s largest vacuum chamber to simulate spaceflight as well as being subjected to acoustic tests to simulate the intense vibrations Orion will endure when launched on the world’s largest rocket, NASA’s Space Launch Systems.

- Second module getting ready: Meanwhile technicians in Bremen are not resting as work on the second European Service Module is already well under way. The structure is complete and over 11 km of cables are being meticulously placed in preparation for the computers and equipment that will keep astronauts alive and well for the second Orion mission called Exploration Mission-2.