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HTV-7(H-II Transfer Vehicle-7 / Kounotori-7)

Launch    HTV-7 Payload     HSRC Mission     References

HTV-7 will be the seventh flight of the HTV (H-II Transfer Vehicle) of JAXA (Japan Aerospace Exploration Agency), an unmanned cargo spacecraft to the ISS (International Space Station). On 28 July 2018, the HTV-7 "Kounotori-7" vehicle was unveiled to media at JAXA's Tanegashima Space Center (TNSC) along with the briefing of its upcoming mission. 1)

Overview of HTV missions: The HTV is launched from the Tanegashima Space Center aboard an H-IIB launch vehicle with up to 6,000 kg of supplies. When the HTV approaches close to the ISS, the Space Station Remote Manipulator System (SSRMS), known as "Canadarm2," grapples the HTV and berth it to the ISS. After the supplies, such as food, clothes and a variety of experiment equipment, are unloaded, the HTV will then be loaded with waste materials, including used experiment equipment or used clothes. The HTV will then undock and separate from the ISS and reenter the atmosphere. While the HTV is berthed to the ISS, the ISS crew will be able to enter and remove the supplies from the HTV Pressurized Logistics Carrier.

Length

~ 10.0 m

Diameter

~ 4.4 m

Mass of vehicle excluding cargo

~ 10,500 kg

Cargo capacity (supplies and equipment)

Total: 6,000 kg maximum
PLC (Pressurized Logistics Carrier): 4,500 kg
ULC (Unpressurized Logistics Carrier): 1,500 kg

Total mass

16,500 kg maximum

Reentry cargo capacity

6,000 kg maximum

Propellant

Fuel: MMH (Monomethylhydrazine)
Oxidizer: MON3 (NTO containing 3wt% NO)

Insertion orbit

Altitude: 350km-460km, Inclination: 51.6 degrees

Mission Duration

Solo flight: Normally 5 days
Berthing: Maximum 45 days
Stand-by (on orbit): Normally 7 days

Table 1: Nominal HTV specifications

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Figure 1: Photo of the HTV-7 vehicle, photographed in the TNSC SFA2 (Fairing Assembly Building 2), image credit: JAXA

The H-II Transfer Vehicle (HTV) consists of two logistic carriers, the PLC (Pressurized Logistics Carrier ) and the ULC (Unpressurized Logistics Carrier), which also includes the EP (Exposed Pallet), as well as an Avionics Module and a Propulsion Module.

The Japanese Experiment Module (JEM), known as "Kibo," is equipped with antennas, reflectors and a Proximity Communication System (PROX) that enables inter-orbit communication with the HTV as the HTV approaches the ISS.

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Figure 2: Nominal configuration of the HTV interior elements (image credit: JAXA)

The PLC carries cargo such as International Standard Payload Racks (ISPRs), drinking water and clothes that will be used aboard the ISS. The PLC's internal air pressure is controlled and maintained at one atmospheric pressure (1 atm). While the HTV is berthed with the ISS, the ISS crew can enter the PLC to unload the supplies. After the supplies are unloaded, waste material will be loaded. The ISS crew members enter and exit through the HTV's berthing port that is equipped with the Common Berthing Mechanism (CBM).

The ULC carries unpressurized cargo loaded on the Exposed Pallet (EP).

The Avionics Module contains navigational and electrical systems used for HTV's navigation control, communication and supplying power. The Avionics Module enables the HTV flight to navigate by receiving commands sent from the ground or to navigate by HTV autonomous flight systems. In addition, the Avionics Module distributes power to each of its components.

The Propulsion Module has four propellant tanks. The HTV's thrusters generate propulsion for orbital adjustment or attitude control. There are 32 thrusters installed on the HTV.

The Proximity Communication System (PROX), which is installed on Kibo, consists of a PROX antenna, a PROX-GPS antenna, PROX communication equipment and a Hardware Command Panel (HCP). With the exception of the PROX antenna, the PROX-GPS antenna and the HCP, the PROX is installed in the JEM Pressurized Module.

When the HTV approaches close to the ISS, the PROX antenna initiates communications with the HTV. This antenna contains GPS receivers. Through the PROX, the ISS's orbital location and speed are immediately relayed to the HTV. At the same time, data from the HTV are relayed to the ISS. In addition, the antenna relays commands sent from the ground to the HTV.

The reflectors are installed on the nadir (bottom) side of Kibo. The reflectors reflect the lasers that are beamed from the HTV's Rendezvous Sensor (RVS) during the HTV close proximity operation.


Launch: MHI ( Mitsubishi Heavy Industries, Ltd.) and JAXA will launch the H-IIB Launch Vehicle No. 7(H-IIB F7) which carries aboard the H-II Transfer Vehicle "Kounotori-7", the cargo transporter to the ISS. The launch is scheduled for 11 September 2018, the launch site is the Yoshinobu Launch Complex at the JAXA TNSC (Tanegashima Space Center), Japan. 2)

Orbit: Near-circular orbit of the ISS, altitude of ~400 km, inclination = 51.6º, period of ~ 93 minutes.



 

HTV-7 Payload

HTV-7 delivers a total of 6.2 metric tons of cargo to the ISS, including 4.3 metric tons in the PLC (Pressurized Logistic Carrier ) and 1.9 metric tons on the ULC (Unpressurized Logistic Carrier).This Kounotori-7 flight is planned to test a new reentry capsule, HSRC (HTV Small Reentry Capsule), developed at JAXA. 3)

Cargo in the PLC (Pressurized Logistic Carrier)

• Two US experiment racks (Express Rack 9B and 10B). The US EXPRESS Racks 9B and 10B will be delivered on this flight. These two EXPRESS Racks are modified for more simple interfaces.

• US Life Sciences Glovebox (LSG): The second ISS large-scale glovebox for scientific experiments, will be installed on board "Kibo".

• LSR (Life Support Rack): The LSR, developed by ESA, is equipment for demonstration test of effective life support system which produces oxygen (O2) from water (H2O) by using electrolysis and also converts the produced hydrogen (H2) in Sabatier reaction with carbon dioxide (CO2), removed from the inside of the cabin, into methane (CH4) and byproduct water (H2O), which is then recycled for electrolysis.

- The rack, also known as ACLS (Advanced Closed Loop System) has been developed by Airbus for ESA as a technology demonstrator, which will purify air and produce oxygen for the ISS. The rack will be installed into the Destiny Module (US Laboratory) by ESA astronaut and ISS commander Alexander Gerst on 2 November 2018. Its technology is a critical step forward towards a closed loop life support system, necessary for human spaceflight beyond low Earth orbit. 4)

- A newly formed ACLS operations team (OPS), based at Airbus in Friedrichshafen, Germany, will operate the ACLS throughout its mission. ACLS OPS is part of the ISS's ground network, and works directly with the ESA Columbus Control Center in Oberpfaffenhofen, Germany.

- Following installation, the ACLS OPS team will commence a six week commissioning phase to check the new facility. Successful commissioning will be followed by operations on the ISS until the end of 2019, with the ACLS providing additional carbon dioxide removal and oxygen generation capabilities to the astronauts onboard.

HSRC (HTV Small Reentry Capsule): The HSRC will demonstrate the newly dveloped reentry technology and cargo recovery function from the ISS. The HSRC, including experiment samples, will be attached to the hatch of the PLC (Pressurized Logistic Carrier) before the HTV-7 unberthing from ISS. HSRC will be separated from the HTV-7 after its deorbit burn; reenter Earth's atmosphere; descend by parachute; and be recovered after splashdown (Figure 5). 5)

- In the HTV-7 mission, after completing the re-supply mission to ISS, HTV-7 will demonstrate the novel technology for recovering experiment samples from ISS, which Japan has not obtained up until now, by taking advantage of the opportunity of reentry into Earth with the HSRC that will be loaded on the HTV for the first time ever.

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Figure 3: Illustration of the HSRC (HTV Small Reentry Capsule), image credit: JAXA

• Loop Heat Pipe Radiator (LHPR) technology demonstration system: The LHPR is expected for high efficiency heat rejection technology for future spacecraft. This LHPR demonstration will perform on-orbit technology demonstration of an expansion-type radiator equipped with a loop heat pipe by using "Kibo" as a test bed environment. — The demonstration aims to reduce risks in satellite development by reflecting the results obtained by the on-orbit demonstration to the design of the expansion-type radiator, which will be applied to Engineering Test Satellite-9 aimed at the realization of next-generation geostationary communications satellites.

• J-SSOD (JEM Small Satellite Orbital Deployer) and CubeSats: This mission will mark the 10th CubeSat deployment system, using the J-SSOD since 2012.

CubeSats: HTV-7 will deliver the following CubeSats developed by a joint team of Nanyang Technological University (NTU, in Singapore) and Kyushu Institute of Technology ("Kyutech", in Japan), general incorporated association Rymansat Spaces, and Shizuoka University.

- SPATIUM-I (Space Precision Atomic-clock TIming Utility Mission-I) of the Kyushu Institute of Technology (Japan)/Nananyang Technological University , Singapore. The 2U CubeSat will perform a mission to demonstrate technology aimed at electron density measurement and three-dimensional mapping of ionosphere and using an ultra-small CASC (Chip Scale Atomic Clock) for CubeSats.

- RSP-00: The 1U CubeSat will perform a mission to demonstrate technology aimed at electron density measurement and three-dimensional mapping of ionosphere and chip scale (ultra-small) atomic clock for CubeSats.

- STARS-Me (Shizuoka University): Two 1U CubeSats will perform small-scale demonstration of a space elevator, which is a demonstration mission of configuration of two satellites and a climber (moving mechanism).

• Fresh food: Following HTV-5 and HTV-6, HTV-7 will also deliver food and other supplies including fresh food.

Cargo on the ULC (Unpressurized Logistic Carrier)

• Following the HTV-6, the HTV-7 (and also HTV8 and HTV9) will deliver new lithium ion batteries for the ISS on the Exposed Pallet (EP) on the ULC. New six battery ORUs (Orbital Replacement Units), consisting of new lithium-ion battery cells, manufactured by a Japanese company, are delivered.

- The nickel-hydrogen batteries currently used on the ISS are becoming old. The extension of ISS operations becomes possible with the supply of Japanese lithium-ion battery cells. Only the HTV is capable of delivering six battery ORUs at one time, and thus plays an important role in continuous ISS operations.

- Since the station is often not in direct sunlight, it relies on rechargeable batteries to provide continuous power during the "eclipse" part of the orbit (35 minutes of every 90 minute orbit). The batteries ensure that the station is never without power to sustain life-support systems and experiments. During the sunlit part of the orbit, the batteries are recharged.

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Figure 4: Photo of the ORU lithium-ion batteries (image credit: JAXA)



 

HSRC mission

The HSRC with experiment samples on board will be attached onto the hatch of the Pressurized Logistic Carrier (PLC) of the HTV-7 before the HTV-7 departs (un-berthed) from ISS. After the HTV-7 deorbit burn finished, the capsule will be released from the PLC by the command from the ground and reenter into Earth's atmosphere, and subsequently descend on a parachute. The capsule will be recovered from the ocean after splashdown.

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Figure 5: Conceptual diagram of HSRC operations (image credit: JAXA)

HSRC and its payload container overview

The HSRC on board HTV-7 "Kounotori-7", where samples will be kept cool in a passive way (no electric cooler), houses a vacuum double layer insulation container (thermos bottle) and a heat storage unit (refrigerant), inside of which experiment samples will be stored.

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Figure 6: Cross section image of HSRC (image credit: JAXA)

Installation of the reentry capsule

Before the HTV-7 departs from the ISS, the crew will load an HSRC-exclusive structure (cylindrical support) onto the hatch at the entry of the Pressurized Logistic Carrier for air tightness (while the hatch of the HTV-7 is left open). The HSRC with the separation mechanism attached will be fixed onto the structure.

After completing the de-orbit maneuver, the HTV-7 will operate the separation mechanism of the HSRC according to the command received from the ground to separate the HSRC from the vehicle.

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Figure 7: Conceptual diagram of installing the HSRC on board the HTV (image credit: JAXA)

The HSRC will reenter Earth's atmosphere in a guided lift flight, deploy a parachute, and splash down into the sea, which in turn be picked up by a recovery ship. Experiment samples taken out from the HSRC will be loaded onto an airplane on Minamitori Island, immediately delivered to the mainland of Japan (the HSRC itself will remain aboard the recovery ship to be delivered to the mainland).



1) "HTV7 media briefing at Tanegashima Space Center," JAXA, 5 September 2018, URL: http://iss.jaxa.jp/en/htv/mission/htv-7/news/180728_htv7_unveil.html

2) "Launch Schedule of the H-II Transfer Vehicle KOUNOTORI7 aboard the H-IIB Vehicle No. 7," JAXA Press Release, 13 July 2018, URL: http://global.jaxa.jp/press/2018/07/20180713_h2bf7.html

3)"HTV-7 Payload," JAXA, 5 September 2018, URL: http://iss.jaxa.jp/en/htv/mission/htv-7/payload/

4) "Airbus-built ACLS Life Support Rack is ready for launch from Tanegashima," Space Daily, 6 September 2018, URL: http://www.spacedaily.com/reports
/Airbus_built_ACLS_Life_Support_Rack_is_ready_for_launch_from_Tanegashima_999.html

5) "HTV Small Re-entry Capsule," JAXA, 5 September 2018, URL:
http://iss.jaxa.jp/en/htv/mission/htv-7/hsrc/index.html
 


The information compiled and edited in this article was provided by Herbert J. Kramer from his documentation of: "Observation of the Earth and Its Environment: Survey of Missions and Sensors" (Springer Verlag) as well as many other sources after the publication of the 4th edition in 2002. - Comments and corrections to this article are always welcome for further updates (herb.kramer@gmx.net).

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