Minimize IRIS

IRIS (Interface Region Imaging Spectrograph) Observatory

Overview    Spacecraft    Launch    Mission Status    Sensor Complement   Ground Segment    References

IRIS is a science mission in NASA's SMEX (Small Explorer) program to study the interface between the photosphere and corona of the sun. The IRIS investigation is centered on three themes of broad significance to solar and plasma physics, space weather, and astrophysics, aiming to understand how internal convective flows power atmospheric activity:

1) Which types of non-thermal energy dominate in the chromosphere and beyond?

2) How does the chromosphere regulate mass and energy supply to corona and heliosphere?

3) How do magnetic flux and matter rise through the lower atmosphere, and what role does flux emergence play in flares and mass ejections?

The complex processes and enormous contrasts of density, temperature and magnetic field within this interface region require instrument and modeling capabilities that are only now within reach. The IRIS team will use advances in instrumental and computational technology, its extensive experience, and its broad technological heritage to build a state-of-the-art instrument to provide unprecedented access to the plasma-physical processes in the interface region. 1) 2) 3)

IRIS will provide key insights into all these processes, and thereby advance our understanding of the solar drivers of space weather from the corona to the far heliosphere, by combining high-resolution imaging and spectroscopy for the entire chromosphere and adjacent regions. IRIS will resolve in space, time, and wavelength the dynamic geometry from the chromosphere to the low-temperature corona to shed much-needed light on the physics of this magnetic interface region.

In June 2010, NASA selected the IRIS mission proposal of LMATC (Lockheed Martin Advanced Technology Center, Palo Alto, CA (PI: Alan M. Title). The IRIS mission uses a solar telescope and spectrograph to explore the solar chromospheres. This is a crucial region for understanding energy transport into the solar wind and an archetype for stellar atmospheres. Recent discoveries have shown the chromosphere is significantly more dynamic and structured than previously thought. The unique instrument capabilities, coupled with state of the art 3-D modeling, will explore this dynamic region in detail. The mission will greatly extend the scientific output of existing heliophysics spacecraft that follow the effects of energy release processes from the sun to Earth. 4) 5) 6) 7)

The IRIS science investigation includes the following team members:

Lockheed Martin Solar and Astrophysics Lab (LMSAL); Lockheed Martin Sensing and Exploration Systems (LMS&ES), SAO (Smithsonian Astrophysical Observatory), Cambridge, MA, USA; MSU (Montana State University), Bozeman, MT, USA; Institute for Theoretical Astrophysics, UiO (University of Oslo), Norway; HAO (High Altitude Observatory) of NCAR, Boulder, CO, USA; Stanford University, Stanford, CA, USA, NASA/ARC (Ames Research Center), Mountain View, CA, USA; NASA/GSFC (Goddard Space Flight Center), Greenbelt, MD, USA; NSO (National Solar Observatory), Space Sciences Lab, AURA (Association of Universities for Research in Astronomy), USA; UCB (University of California, Berkeley); PPPL (Princeton Plasma Physics Laboratory), Princeton, NJ, USA; Sydney Institute for Astronomy, University of Sydney, Australia; Center for Plasma Astrophysics, University of Leuven, The Netherlands; MSSL (Mullard Space Science Laboratory), London, UK; RAL (Rutherford-Appleton Laboratory), UK; ESA (European Space Agency); MPS (Max Planck Institute for Solar Research), Katlenburg-Lindau, Germany; NAO (National Astronomical Observatory), Tokyo, Japan; Niels Bohr Institute, University of Copenhagen, Sweden.

Background: The chromosphere and transition region (TR) form a complex interface between the solar surface and corona. Almost all of the mechanical energy that drives solar activity and solar atmospheric heating is converted into heat and radiation within this interface region, with only a small amount leaking through to power coronal heating and drive the solar wind. The chromosphere requires a heating rate that is between one and two orders of magnitude larger than that of the corona. Yet despite the importance of the interface region for solar activity, the heating of the corona, and the genesis of the solar wind, the chromosphere and TR have received much less attention than the photosphere or corona. This is in part because the interface region is highly complex. 8)

The transition between high and low plasma β (the ratio of plasma pressure to magnetic pressure) occurs somewhere between photosphere and corona, so that in the interface region, the magnetic field and plasma compete for dominance (with a variety of impacts on, e.g., waves such as mode coupling, refraction and reflection). Within this region, the density drops by 6 orders of magnitude; the temperature rapidly increases from 5,000 to 1 million K, with strong gradients across the magnetic field evident from high-resolution images of the chromosphere (Figure 1).

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Figure 1: Hα line center image taken at the Swedish Solar Telescope on 16-June-2003 showing the fine scale structuring of the upper chromosphere, with the thinnest fibrils having diameters less than 200 km (image credit: LMSAL)

The plasma transitions from partially ionized in the chromosphere (which leads to a variety of interesting plasma physics effects) to fully ionized in the corona, and shows evidence of supersonic and super-Alfvenic motions. To top it off, the chromosphere is partially opaque, with non- LTE (Local Thermodynamic Equilibrium) effects dominating the radiative transfer, so that interpreting the radiation, and determining the local energy balance and ionization state, is non-intuitive and requires advanced computer models. The highly dynamic nature of the chromosphere, as observed with Hinode and ground-based telescopes, further complicates attempts to better understand the interface region. This is both because high cadence observations are required (better than 15 seconds), and because the ionization state of some elements (e.g., hydrogen) reacts only slowly to changes in the energy balance, and thus depends on the history of the plasma. IRIS will exploit recent advances in novel, high throughput and high-resolution instrumentation, efficient numerical simulation codes, and powerful, massively parallel supercomputers, to open a new window into the physics of the interface region Ref. 8).

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Figure 2: Artist's rendition of the IRIS spacecraft (image credit: NASA)

Spacecraft:

Construction, integration and testing of the IRIS spacecraft will be done by the Lockheed Martin Space Systems ATC (Advanced Technology Center) in Palo Alto, CA. Mission operations and some system engineering will be the responsibility of NASA/ARC.

IRIS is a 3-axis stabilized, sun-pointed mission that studies the chromospheres in the FUV (Far Ultraviolet) and NUV (Near Ultraviolet) spectral region with 0.33 arcsec spatial resolution, 0.4 km/s velocity resolution and a FOV (Field of View) of 171 arcsec. This two-year mission fills a critical observational data gap by providing simultaneous, co-spatial and comprehensive coverage from photosphere (~4,500 K) up to corona (≤ 10 MK). IRIS consists of a 20 cm aperture telescope assembly that feeds an imaging spectrograph and a separate imaging camera system with wavelengths in the FUV and NUV. A spacecraft bus based upon heritage designs (TRACE) supports the science mission and provides pointing, power, and data communications for the mission.

• A guide telescope is used for fine pointing

• The pointing range is anywhere within the 1.2 Rsun from disk center

• RAD 750 CPU

• Power generation of 340 W, 28 V. The two solar arrays measure 0.6 m x 1.3 m each, with a total surface area of 1.7 m2.

• RF communications: X-band for payload downlink at 15 Mbit/s including the overhead of LDPC (Low Density Parity Checking ) 7/8s encoding. The effective downlink rate is 13 Mbit/s (excluding overhead) during up to 15 passes per day with the antennas of KSAT (Kongsberg Satellite Services) in Svalbard, Norway, as well as some passes from NASA's NEN (Near Earth Network) in Alaska and Wallops. Onboard data storage capacity of 48 Gbit in solid state memory. IRIS is equipped with two omnidirectional S-band antennas for uplinking of commands and downlinking of engineering data.The S-band provides uplink at 2 kbit/s and downlink at 256 kbit/s.

There is no propulsion system and there are no consumables on board. The ACS can point the telescope IRIS boresight to any location on the solar disk or above above the limb within 21 arcminutes of disk center, and roll the spacecraft (and thus, the spectrograph slit), up to ±90º (at 0º the slit is oriented parallel to N-S on the Sun).

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Figure 3: Overview of the IRIS observatory showing the 20 cm UV telescope, with and without solar panels (image credit: (NASA, LMSAL) 9)

Mission development: 10)

The cost, schedule, and size constraints were part of all design trades. The result was to use existing hardware and software designs as much as possible and to use commercially supplied components where feasible. Single string systems and subsystems were used throughout the observatory. The observatory was designed for autonomous on-orbit operations with minimal human support from the ground. Flight spares, brassboards, and engineering units were kept to a minimum. Deferral of subsystem testing was carried out to streamline the integration and test effort, and qualification by similarity was used for components with flight heritage. A small core team was responsible for the design, development, integration, test, launch, and on-orbit checkout of the observatory.

For the spacecraft, prior missions and design studies were used for reference in the design of the IRIS spacecraft bus. The LM team designed the spacecraft architecture including the bus structure, the harness and interconnects, the MLI (Multi-Layer Insulation) blanketing, the ACS (Attitude Control Subsystem) flight software, the fault management scheme, and the EGSE (Electrical Ground Support Equipment). The solar arrays, deployment mechanisms, and EGSE were developed in house. The majority of the spacecraft components were procured from vendors with a majority being catalog items such as the reaction wheel assemblies, torque rods, IAU (Integrated Avionics Unit) which consisted of the C&DH and EPS subsystems, the coarse and digital sun sensors, the magnetometer, and the star trackers. The flight and test batteries were spares from the GRAIL program (Ref. 10).

The S-band and X-band RF communications units were vendor developed to meet the system requirements and size constraints of the IRIS spacecraft structure. Cost and schedule saving features included the design of a gyro-less ACS system enabled by the use of the fine pointing signal from the instrument guide telescope and the use of auto generated ACS code from the Simulink system model. The only engineering units procured for the spacecraft development were two IAU engineering models used for development and test of the spacecraft and ACS software. The communications vendor developed engineering units for the X- and S- band units to aid in their development, but they were not contract deliverables.

A RWA (Reaction Wheel Assembly) engineering unit was loaned from the GRAIL program to aid in an anomaly investigation, but was not transferred to the IRIS program and the magnetometer vendor loaned an engineering unit for system and model validation. No spacecraft flight spares were procured. The architecture was single string with some limited redundancy from the use of 4 RWAs (Reaction Wheel Assemblies, can operate in degraded mode with 3) and the star tracker and magnetometer electronics units.

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Figure 4: Spacecraft schematic (image credit: LMSAL)

The assembly, integration, and test operations were also planned with cost, schedule, and risk in mind. The traditional flight development program would have a progressive level of flight qualification and acceptance testing as components are developed and integrated into higher levels of assembly. On an enhanced Class D mission such as IRIS, all flight acceptance tests are performed, but the program has the ability to trade at what level the tests are carried out, as long as all subsystems are exposed to the required test environments at some time in the test flow. The majority of the vendor supplied hardware was acceptance tested prior to delivery to LM. One exception was the telescope assembly for which the thermal vacuum, vibration, and EMI/EMC (Electromagnetic Interference/ Electromagnetic Compatibility) tests were deferred to higher levels of assembly.

For the instrument, vibration testing was deferred to the observatory level due to the complexity of replicating the mounting to the spacecraft and to reduce the risk of over test. However, extensive thermal vacuum and optical performance testing was performed at the instrument level due to the new spectrograph design and the complexity of optical stimulation at the observatory level. Instrument level EMI/EMC testing was deferred to the observatory level to ensure all electrical interfaces were tested in the most flight like configuration. For the spacecraft, vibration, thermal vacuum, and EMI/EMC tests were all deferred to the observatory level. The decision as to which level of integration to carry out the environmental and acceptance testing was based on balancing schedule, test complexity, and risk with many of the decisions reducing the overall risk to the mission.

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Figure 5: Photo of the fully integrated IRIS spacecraft in a cleanroom of Lockheed Martin Space Systems (image credit: NASA, Lockheed Martin) 11)

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Figure 6: Photo of the IRIS spacecraft in launch configuration (image credit: NASA, Lockheed Martin)

Spacecraft mass

183 kg observatory (87 kg instrument, 96 kg spacecraft)

Spacecraft size

~ 2.18 m in length,and ~ 3.7 m across with its solar panels deployed

Power

365W Solar Array at BOL (Beginning of Life)

FOV (Field of View)

Imager: 175 arcsec x 175 arcsec
SJI (Slit Jaw Imager): 0.33 arcsec x 175 arcsec
Spectrograph scan: 130 arcsec x 175 arcsec

Resolution

0.4 arcsec NUV (Near Ultraviolet)
0.33 arcsec FUV (Far Ultraviolet)

Science data link

32 Mbit/s

Onboard storage capacity

6 Gbyte

Data volume

> 45 Gbit/day

Design life

2 years

Table 1: Key performance parameters of IRIS

 

Launch: The IRIS spacecraft was launched on June 28, 2013 (2.27 UTC) aboard a Pegasus XL vehicle of OSC (Orbital Sciences Corporation) from VAFB (Vandenberg Air Force Base), CA, USA. The L-1011 aircraft took off from VAFB and flew to the drop point over the Pacific Ocean, where the aircraft released the Pegasus XL from beneath its belly. 12) 13)

Orbit: Sun-synchronous orbit, altitude of 620 km x 670 km, inclination = 97.9º. The orbit allows eclipse-free continuous viewing for 7 months per year. The instrument will not be operated in the 4 months in which eclipses occur.

NASA/ARC (Ames Research Center), Moffett Field, CA, is responsible for mission operations and the ground data system. The NSC (Norwegian Space Center) captures the IRIS data with their antennas in Svalbard, inside the Arctic Circle, in northern Norway (Spitsbergen). The science data will be managed by the Joint Science Operations Center of the Solar Dynamics Observatory, run by Stanford and Lockheed Martin. NASA's Goddard Space Flight Center in Greenbelt, Md., oversees the SMEX project.

 


 

Mission status:

• Sept. 19,2016: The IRIS mission, built and operated by Lockheed Martin for NASA, has received more time to deliver groundbreaking space science. A new NASA contract extends the Lockheed Martin's support for the orbiting observatory through September 2018, with a further extension possible through September 2019. 14)

- Since its launch in June 2013, IRIS has taken more than 24 million images or spectral measurements of the sun. Scientists at NASA, Lockheed Martin and other institutions around the world have used IRIS to make exciting discoveries about what causes the heating of the solar atmosphere and how solar flares are triggered and release magnetic energy. The observatory views only a small part of the sun at any time, but through careful planning by the IRIS science planning team, IRIS was able to catch nine of the largest flares (X-class) and almost 100 of the second largest class of flares (M-class) and numerous weaker C-class flares.

• On July 24, 2016, NASA's IRIS (Interface Region Imaging Spectrograph) satellite captured a mid-level solar flare: a sudden flash of bright light on the solar limb – the horizon of the sun – as seen at the beginning of this video. Solar flares are powerful explosions of radiation. During flares, a large amount of magnetic energy is released, heating the sun's atmosphere and releasing energized particles out into space. Observing flares such as this helps the IRIS mission study how solar material and energy move throughout the sun's lower atmosphere, so we can better understand what drives the constant changes we can see on our sun. 15)

- As the video continues, solar material cascades down to the solar surface in great loops, a flare-driven event called post-flare loops or coronal rain. This material is plasma, a gas in which positively and negatively charged particles have separated, forming a superhot mix that follows paths guided by complex magnetic forces in the sun's atmosphere. As the plasma falls down, it rapidly cools – from millions down to a few tens of thousands of kelvins. The corona is much hotter than the sun's surface; the details of how this happens is a mystery that scientists continue to puzzle out. Bright pixels that appear at the end of the video aren't caused by the solar flare, but occur when high-energy particles bombard IRIS's CCD device camera – an instrument used to detect photons.

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Figure 7: Photo of a mid-sized flare on the solar limb, acquired by IRIS on July 24, 2016 (image credit: NASA/GSFC)

• The IRIS spacecraft and its payload are operating nominally in 2016. 16)

• July 2015: The IRIS mission is approved by NASA to continue its first extended mission and to plan against the current budget guidelines. Any changes to the guidelines will be handled through the budget formulation process. The IRIS mission will be invited to the 2017 Heliophysics Senior Review. 17)

- The IRIS (Interface Region Imaging Spectrograph) Observatory provides spectra and images from the solar photosphere into the low corona. It is designed to make spectroscopic observations of the Sun at high spatial, spectral, and temporal resolution. The spacecraft carries a 20 cm UV Cassegrain telescope that feeds a dual range UV slit spectrograph and slit-jaw imager. IRIS has an effective spatial resolution between 0.33 and 0.44 arcseconds, and a maximum field of view of 120 arcseconds. The far-UV channel covers the 133.0–141.0 nm range, with a 4 x 10-3 nm spectral resolution. The near-UV channel covers the 278.0–284.0 nm range, with an 8 x 10-3 nm spectral resolution. The slit-jaw imaging covers similar ranges in the far-UV (4.0 nm bandpass) and near-UV (0.4 nm bandpass). IRIS has a very high data rate, that allows images to be taken every 5–10 s and spectra every 1–2 s. IRIS travels in a polar sun-synchronous orbit (twilight orbit) that allows for eight months of continuous observations per year and maximizes eclipse-free viewing of the Sun.

- On June 28, 2015, the IRIS observatory was 2 years on orbit. IRIS observations have advanced our understanding of what role the interface region, which lies between the sun's photosphere and corona, plays in powering its dynamic million-degree atmosphere and driving the solar wind. Since its first birthday last summer, IRIS data has revealed unexpected complexity in the interface region and investigated the source of the extremely high temperatures of the solar atmosphere, or corona. 18)

• June 2015: The 2015 Heliophysics Senior Review panel undertook a review of 15 missions currently in operation in April 2015. The panel found that all the missions continue to produce science that is highly valuable to the scientific community and that they are an excellent investment by the public that funds them. 19)

- The IRIS mission deliberately combines unprecedented observations of the solar chromosphere and transition region with advanced numerical simulations, including the development of publicly available sophisticated radiative transfer codes. During its prime mission phase IRIS has already achieved significant milestones in reaching its primary objective of understanding the processes that energize the solar atmosphere. For example, the detection of non-thermal electrons in coronal nano-flares provides new insight into mechanisms behind non-thermal energy generation specifically which dominate in the chromosphere and corona. The IRIS high-resolution spectra have shown for the first time the existence of regions of very dense plasma in the photosphere and low chromosphere that are rapidly accelerated and heated to 80,000 K. This discovery has pushed numerical simulations to explore specific reconnection processes that will explain these newly observed features and their impact regarding the mass and energy supply for the corona. One of the most challenging problems in solar physics today is to better understand the nature of solar flares and CMEs (Coronal Mass Ejections). IRIS has provided critical data that demonstrate, for example, the important role played by electron beams in the chromosphere during flares (which challenges some flare models) and evidence for tether-cutting magnetic reconnection as a trigger for both flares and associated CMEs.

- The IRIS Science Plan for its extended phase is quite compelling. It is focused on five prioritized science goals: 1) Study the fundamental physical processes in the solar atmosphere; 2) Investigate the (in)stability of the magnetized atmosphere; 3) Analyze the energy and mass transfer between photosphere, chromosphere, and corona; 4) Quantify the variations of far and near ultraviolet solar radiation over the solar cycle; 5) Explore the solar-stellar connection. The accomplishment of these goals will provide a new insight into basic physical processes and improve the current numerical models.

- IRIS Science Strengths: IRIS provides the highest spectral resolution observations of the chromosphere and transition region in the far-UV and near-UV ranges of any mission. The subarcsecond spatial resolution combined with the very high temporal cadence of the observations makes IRIS a unique instrument for detailed studies of the magnetic field reconnection and its thermodynamic effects in flares. IRIS has a strong program of coordinated observations with Solar-B/Hinode and SDO (Solar Dynamics Observatory). IRIS chromospheric and transition region spectra and images form a perfect complement to Hinode's high-resolution photospheric magnetograms and coronal spectra and images, and to SDO's contextual full-disk magnetograms and coronal images. The synergy with Hinode and SDO allows studies of how the magnetic field drives and mediates dynamics and heating in the coronal and solar wind. The high quality of the data and the new research opportunities offered by this mission are confirmed by 31 refereed papers published in the 16 months since the data became public, a rate similar to the corresponding phase of other Heliophysics missions.

- The research topics outlined in the proposal are highly relevant to the heliophysics research objectives. During its extended phase the IRIS mission will focus in further developing advanced numerical simulations to improve the diagnostic value of its observations, and further strengthening collaborations with other spaceborne and ground-based observatories. IRIS science goals for the next five years will address a broad range of unsolved questions pertinent to the physics of the solar chromosphere and low corona, such as which physical processes dominate the heating of the chromosphere, which mechanisms drive white light flares and initiate coronal mass ejections, and how jets supply mass to the corona and to the fast/slow solar wind. The transition layers of the solar atmosphere are crucial to understand in terms of the basic physics of our star, but they are so highly structured and dynamic that only the unique capabilities of the IRIS mission are presently poised to provide answers.

- IRIS is a great asset to the HSO (Heliophysics Systems Observatory). It has an excellent track record of coordinating with HSO missions. The current synergy with Hinode, SDO and RHESSI is an example of a system's approach to build up a better understanding of such a complex system as the solar atmosphere. Future collaboration/coordination plans include ground-based instrumentation that will soon be operational, such as the ALMA (Atacama Large Millimeter/submillimeter Array), the German GREGOR 1.6 m telescope, and the NSF-funded 4 m DKIST (Daniel K. Inouye Solar Telescope). IRIS observations will be used to investigate solar abundance details and provide physical insight into the cyclic- and feature-driven variability of the solar UV output—both of which have far-reaching impact in heliospheric and astrophysical science.

- IRIS spacecraft / instrument health and status: The IRIS spacecraft contains no consumables, and has performed almost flawlessly on orbit for two years. No subsystem shows signs of significant degradation.

- IRIS Data Operations (accessibility, quality control, archiving) The IRIS data are available to the science community in each level of reduction as soon as they are available at the SDO JSOC (Joint Science Operations Center), where they are archived and processed. Calibrated data are available within seven days of the observations, while preliminary calibrated quick-look images are provided within hours of the observations. The Heliophysics Coverage Registry provides a specific search engine that enables easy co-temporal/spatial IRIS and Hinode data comparison. In addition, the modeling output are considered part of the IRIS mission data and made available for community analysis through the same distribution channel.

• On May 6, 2015, the IRIS mission completed its 10,000th orbit of the Earth. On June 27, 2015, IRIS was two years on orbit. 20)

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Figure 8: In this photo, the IRIS spacecraft captured several large solar prominences on the edge of the sun, acquired on April 28, 2015 (image credit: NASA)

• October 16, 2014: The IRIS mission has provided scientists with five new findings into how the sun's atmosphere, or corona, is heated far hotter than its surface, what causes the sun's constant outflow of particles called the solar wind, and what mechanisms accelerate particles that power solar flares. - The new information will help researchers better understand how our nearest star transfers energy through its atmosphere and track the dynamic solar activity that can impact technological infrastructure in space and on Earth. 21) 22)

Five papers, based on IRIS data, highlight different aspects of the energy's journey from the sun's surface through its atmosphere in the Oct. 17, 2014, issue of Science magazine. 23)

- Solar heat bombs: The first result identified heat pockets of 200,000 degrees Fahrenheit (~111100º C), lower in the solar atmosphere than ever observed by previous spacecraft. Scientists refer to the pockets as solar heat bombs because of the amount of energy they release in such a short time. Identifying such sources of unexpected heat can offer deeper understanding of the heating mechanisms throughout the solar atmosphere.

- Resolving unresolved structure: For its second finding, IRIS observed numerous, small, low lying loops of solar material in the interface region for the first time. The unprecedented resolution provided by IRIS will enable scientists to better understand how the solar atmosphere is energized.

- Mini-tornadoes: A surprise to researchers was the third finding of IRIS observations showing structures resembling mini-tornadoes occurring in solar active regions for the first time. These tornadoes move at speeds as fast as 20 km/s and are scattered throughout the chromosphere, or the layer of the sun in the interface region just above the surface. These tornados provide a mechanism for transferring energy to power the million-degree temperatures in the corona.

- High-speed jets: Another finding uncovers evidence of high-speed jets at the root of the solar wind. The jets are fountains of plasma that shoot out of coronal holes, areas of less dense material in the solar atmosphere and are typically thought to be a source of the solar wind.

- Accelerated electrons in nanoflares: The final result highlights the effects of nanoflares throughout the corona. Large solar flares are initiated by a mechanism called magnetic reconnection, whereby magnetic field lines cross and explosively realign. These often send particles out into space at nearly the speed of light. Nanoflares are smaller versions that have long been thought to drive coronal heating. IRIS observations show high energy particles generated by individual nanoflare events impacting the chromosphere for the first time.

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Figure 9: Illustration of ubiquitous nanoflares throughout the corona (image credit: NASA)

• August 2014: The science and technical performance of the observatory has been excellent. All systems are currently operating within specification and the science continues to exceed level one requirements. The observatory operates and executes the science timelines autonomously with the MOC uploading commands via S-band once per day, five days a week. The science team develops the timelines based on recent active areas and regions of interest and based on collaborations with other missions and observatories; the timelines are loaded between one and three days before execution. The science data is transmitted to the ground via X-band using ground stations at Svalbard, Alaska, and Wallops. The data is transmitted via internet protocol to the MOC and then to Stanford for archiving, processing, and distribution to the science community (Ref. 10).

- The technical performance on-orbit has met or exceeded the program requirements. The ACS pointing performance of the pitch and yaw axis during nominal science operations has been better than 0.5 arcsec, which is an order of magnitude better than the requirements. The peak to peak roll error is 7.7 arcsec which translates to a line of sight error on the sun to less than 0.05 arcsec. While there are periodic disturbances from the large filter wheel in the instrument and from RWA momentum unloading, these motions are corrected by the instrument's image stabilization system.

- Over the past year, IRIS has carried out greater than 5000 orbits of solar observations including long observations of active regions and studies of: coronal holes, solar plage, solar flares, emergence of filaments, spicules, coronal rain, and other solar features.

• June 28, 2014: One year ago today, NASA's newest solar observatory was launched into orbit around Earth. IRIS observes the low level of the sun's atmosphere — a constantly moving area called the interface region — in better detail than has ever been done before. 24)

- During its first year in space, IRIS provided detailed images of this area, finding even more turbulence and complexity than expected. The interface region lies at the core of many outstanding questions about the sun's atmosphere, such as how solar material in the corona reaches millions of degrees, several thousand times hotter than the surface of the sun itself or how the sun creates giant explosions like solar flares and coronal mass ejections. The interface region is also where most of the ultraviolet emission is generated that impacts the near-Earth space environment and Earth's climate.

- In its first year, IRIS fortuitously witnessed dozens of solar flares, including one X-class flare, and the foot points of a coronal mass ejection, or CME. IRIS must commit to pointing at certain sections of the sun at least a day in advance, so catching these eruptions in the act involves educated guesses and a little bit of luck.

- There have been several CMEs during the past year, but, due to the small field of view, IRIS must be pointed at the location when the CME occurs as finally happened on May 9, 2014.

• A CME (Coronal Mass Ejection) surged off the side of the sun on May 9, 2014, and NASA's newest solar observatory caught it in extraordinary detail. This was the first CME observed by IRIS. 25)

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Figure 10: First CME observed by IRIS on May 9, 2014 (image credit: LMSAL)

Legend to Figure 10: The four panels show the evolution of the CME as captured in the SJI channel; the sequence starts in the top left panel and progresses from frame a-d. The images cover a 175 arcsec x 175 arcsec area of the sun. The central line is the 0.33 arcsec wide spectrograph slit.

• On March 29, 2014, an X-class flare (CME) erupted from the right side of the sun... and vaulted into history as the best-observed flare of all time. The flare was witnessed by four different NASA spacecraft and one ground-based observatory — three of which had been fortuitously focused in on the correct spot as programmed into their viewing schedule a full day in advance. 26)

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Figure 11: This combined image shows the March 29, 2014, X-class flare as seen through the eyes of different observatories. SDO is on the bottom/left, which helps show the position of the flare on the sun. The darker orange square is IRIS data. The red rectangular inset is from Sacramento Peak. The violet spots show the flare's footpoints from RHESSI (image credit: NASA/GSFC)

The telescopes involved were:

- NASA's IRIS (Interface Region Imaging Spectrograph)

- NASA's SDO (Solar Dynamics Observatory)

- NASA's RHESSI (Reuven Ramaty High Energy Solar Spectroscopic Imager)

- JAXA's Solar-B/Hinode Observatory

- National Solar Observatory's Dunn Solar Telescope located at Sacramento Peak in New Mexico.

Numerous other spacecraft provided additional data about what was happening on the sun during the event and what the effects were at Earth.

- NASA's STEREO mission and the SOHO mission of ESA and NASA both watched the great cloud of solar material that erupted off the sun with the flare.

- NOAA's GOES satellite tracked X-rays from the flare, and other spacecraft measured the effects of the flare as it came toward Earth.

This event was particularly exciting for the IRIS team, as this was the first X-class flare ever observed by IRIS (launched on June 28, 2013). IRIS provided scientists with the first detailed view of what happens in this region during a flare.

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Figure 12: X1-class solar flare on March 29, 2014 as seen by NASA's IRIS spacecraft (image credit: NASA/IRIS/SDO) 27)

Coordinated observations are crucial to understanding such eruptions on the sun and their effects on space weather near Earth. Where terrestrial weather watching involves thousands of sensors and innumerable thermometers, solar observations still rely on a mere handful of telescopes. The instruments on the observatories are planned so that each shows a different aspect of the flare at a different heights off the sun's surface and at different temperatures. Together the observatories can paint a three-dimensional picture of what happens during any given event on the sun.

• On Jan. 28, 2014, NASA's IRIS (Interface Region Imaging Spectrograph) mission witnessed its strongest solar flare since it launched in the summer of 2013. Solar flares are bursts of X-rays and light that stream out into space, but scientists don't yet know the fine details of what sets them off.

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Figure 13: On Jan. 28, 2014, the IRIS observatory observed its strongest solar flare to date (image credit: NASA/GSFC, IRIS, SDO)

- IRIS peers into a layer of the sun's lower atmosphere just above the surface, called the chromosphere, with unprecedented resolution. However, IRIS can't look at the entire sun at the same time, so the team must always make decisions about what region might provide useful observations. On Jan. 28, scientists spotted a magnetically active region on the sun and focused IRIS on it to see how the solar material behaved under intense magnetic forces. At 19:40 UTC, a moderate flare, labeled an M-class flare — which is the second strongest class flare after X-class — erupted from the area, sending light and X-rays into space. 28)

- IRIS studies the layer of the sun's atmosphere called the chromosphere that is key to regulating the flow of energy and material as they travel from the sun's surface out into space. Along the way, the energy heats up the upper atmosphere, the corona, and sometimes powers solar events such as this flare.

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Figure 14: NASA's IRIS witnessed its strongest solar flare since it launched in the summer of 2013 (image credit: NASA, IRIS)

• December 2013: Over its first six months, IRIS has thrilled scientists with detailed images of the interface region, finding even more turbulence and complexity than expected. IRIS scientists presented the mission's early observations at a press conference at the Fall American Geophysical Union meeting in San Francisco, CA, on Dec. 9, 2013. 29) 30) 31)

For the first time, IRIS is making it possible to study the explosive phenomena in the interface region in sufficient detail to determine their role in heating the outer solar atmosphere. The mission's observations also open a new window into the dynamics of the low solar atmosphere that play a pivotal role in accelerating the solar wind and driving solar eruptive events.

Tracking the complex processes in the interface region requires instrument and modeling capabilities that are only now within our technological reach. IRIS captures both images and what's known as spectra, which display how much of any given wavelength of light is present. This, in turn, corresponds to how much material in the solar atmosphere is present at specific velocities, temperatures and densities. IRIS's success is due not only to its high spatial and temporal resolution, but also because of parallel development of advanced computer models. The combined images and spectra have provided new imagery of a region that was always known to be dynamic, but shows it to be even more violent and turbulent than imagined.

The project is seeing rich and unprecedented images of violent events in which gases are accelerated to very high velocities while being rapidly heated to hundreds of thousands of degrees. Bart De Pontieu, the IRIS science lead at Lockheed Martin, has been culling images of two particular types of events on the sun that have long been interesting to scientists.

- One is known as a prominence, which are cool regions within the interface region that appear as giant loops of solar material rising up above the solar surface. When these prominences erupt they lead to solar storms that can reach Earth. IRIS shows highly dynamic and finely structured flows sweeping throughout the prominence.

- The second type of event is called a"spicule", which are giant fountains of gas – as wide as a state and as long as Earth – that zoom up from the sun's surface at 150,000 miles per hour. Spicules may play a role in distributing heat and energy up into the sun's atmosphere, the corona. IRIS imaging and spectral data allows the project to see at high resolution, for the first time, how the spicules evolve. In both cases, observations are more complex than what existing theoretical models predicted.

Mats Carlsson of the University of Olso helps support the crucial computer model component of IRIS' observations. The computer models require an intense amount of power. Modeling just an hour of events on the sun can take several months of computer time. IRIS relies on supercomputers at NASA/ARC, the Norwegian supercomputer collaboration and the Partnership for Advanced Computing in Europe.

Such computer models had helped design the IRIS instruments by providing a basis for the instrument performance requirements. Currently, they are used for analysis of IRIS data, as they represent the state of knowledge about what scientists understand about the interface region. By comparing models with actual observations, researchers figure out where the models fail, and therefore where the current state of knowledge is not complete.

IRIS_AutoA

Figure 15: The fine detail in images of prominences in the sun's atmosphere from NASA's IRIS mission – such as the red swirls shown here – are challenging the way scientists understand such events (image credit: NASA, LMSAL, IRIS collaboration)

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Figure 16: IRIS provides novel views of the mass cycle at the interface between the cool surface and hot atmosphere; the image of the active transition region was acquired on Oct. 2, 2013 (image credit: IRIS collaboration, Ref. 29)

• On July 17, 2013, the IRIS team opened the IRIS telescope door and captured its first observations of a region of the sun that is now possible to observe in detail: the lowest layers of the sun's atmosphere (Figure 17). 32) 33) 34)

The first images from IRIS show the solar interface region in unprecedented detail. They reveal dynamic magnetic structures and flows of material in the sun's atmosphere and hint at tremendous amounts of energy transfer through this little-understood region. These features may help power the sun's dynamic million-degree atmosphere and drive the solar wind that streams out to fill the entire solar system.

IRIS capabilities are tailored to let scientists observe the interface region in exquisite detail. The energy flowing through it powers the upper layer of the sun's atmosphere, the corona, to temperatures greater than 1 million ºC. That is almost a thousand times hotter than the sun's surface. Understanding the interface region is important because it drives the solar wind and forms the ultraviolet emission that impacts near-Earth space and Earth's climate.

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Figure 17: These two images show a section of the sun as seen by IRIS (right) and by the SDO mission (left), acquired on July 17, 2013 (image credit: NASA)

• In its first step towards science operations since launch, . 35)

• A 60 day check out period began at launch. The first 30 days, which ended on July 27, consisted of tests and spacecraft system checks. The team will use the remaining 30 days for initial observing runs to fine tune instrument observations. If all is nominal, the team plans to begin normal science mode by August 26, 2013. 36)

IRIS_Auto7

Figure 18: Artist's rendition of the IRIS spacecraft on orbit (image credit: NASA/GSFC)

 


 

IRIS instrument:

The IRIS instrument is a multi-channel imaging spectrograph with a 20 cm UV telescope. The objective is to obtain UV spectra and images with high resolution in space (1/3 arcsec) and time (1s) focused on the chromosphere and the transition region of the sun, a complex dynamic interface region between the photosphere and corona. In this region, all but a few percent of the non-radiative energy leaving the sun is converted into heat and radiation. Here, magnetic field and plasma exert comparable forces, resulting in a complex, dynamic region whose understanding remains a challenge. 37) 38) 39) 40)

The IRIS instrument uses a Cassegrain telescope with a 19 cm primary mirror and an active secondary mirror with a focus mechanism. The telescope has a FOV of about 3 arcmin x 3 arcmin and feeds far UV (FUV, from 1332 to 1407 Å) and near UV (NUV, from 2783 to 2835 Å) light into a spectrograph box. Dielectric coatings throughout the optical path ensure visible and IR radiation is suppressed. Most of the solar energy passes through the ULE substrate of the primary mirror and is radiated back into space.

IRIS_Auto6

Figure 19: Conceptual design of the IRIS instrument (image credit: NASA/LMSAL)

The IRIS telescope is feeding a stigmatic UV spectrograph and a SJI (Slit-Jaw Imager) that provide an unprecedented combination of 1/3 arcsec imaging with rapid high-resolution spectroscopy. Simultaneous intensity and velocity maps (spectroheliograms) in multiple UV emission lines covering a range of chromospheric, transition region, and coronal temperatures are acquired at a cadence that is comparable to pure imaging instruments. The UV slit-jaw imager provides high resolution, high cadence imaging in selected spectral bands. The instrument package builds extensively on heritage technology: TRACE, SXI (GOES), SECCHI-EUVI (STEREO), FPP (Hinode), and HMI/AIA of SDO.

In December 2010, the IRIS instrument passed the CDR (Critical Design Review) conducted at LMSAL (PI: Alan Title). 41) 42)

IRIS_Auto5

Figure 20: Diagram of spectrograph and slit-jaw imager with part of the internal structure and baffling (image credit: NASA/LMSAL)

IRIS_Auto4

Figure 21: The IRIS instrument block diagram (image credit: LMSAL)

IRIS will obtain spectra along a slit (1/3 arcsec wide), and slit-jaw images. The CCD detectors will have 1/6 arcsec pixels. IRIS will have an effective spatial resolution between 0.33 and 0.4 arcsec and a maximum field of view of 120 arcsec.

Primary diameter

19 cm

Effective focal length

6.895 m

FOV (Field of View)

175 arcsec x 175 arcsec of SJI (Slit Jaw Imager), ⅓ arcsec x 175 arcsec (SG – slit), 130 arcsec x 175 arcsec (SG – raster)

Spatial scale (pixel)

0.167 arcsec

Spatial resolution

1/3 arcsec FUV (Far-UV), 0.4 arcsec NUV (Near-UV)

Spectral scale (pixel)

12.8 mÅ (FUV), 25.6 mÅ (NUV)

Spectral resolution

26 mÅ (FUV SG), 53 mÅ (NUV SG)

Bandwidth

55 Å (FUV SJI), 4 Å (NUV SJI)

CCD detectors

Four e2v 2061 x 1056 pixels, thinned, back-illuminated

CCD cameras

Two x 4-port readout cameras (SDO flight spares)

Detector full well

150,000 electrons

Typical exposure times

0.5 to 30 seconds

Flight Computer

BAe RAD 6000

Mass

Instrument = 87 kg, spacecraft = 96 kg, Total = 183 kg

Power

Instrument = 55 W, spacecraft = 247 W, Total = 302 W

Science telemetry

Average downlink rate = 0.7 Mbit/s, X-band downlink rate = 13 Mbit/s, Total data volume ~ 20 GB(day (uncompressed)

Table 2: IRIS instrument characteristics (Ref. 7)

IRIS will have a high data rate (0.7 Mbit/s on average) so that the baseline cadence is: 5 s for slit-jaw images, 1 s for six spectral windows, including rapid rastering to map solar regions.

Band

Wavelength (Å)

Dispersion (mÅ)

FOV
(arcsec)

Pixel
(arcsec)

CEB

Shutter

EA (cm2)

Temperature (log T)

FUV1

1331.7-1358.4

12.98

175

0.16632

1

FUV SG

1.6

3.7-7.0

FUV 2

1389.0-1407.0

12.72

175

0.16632

1

FUV SG

2.2

3.7-5.2

NUV

2782.7-2835.1

25..46

175

0.16637

2

NUV SG

0.2

3.7-4.2

Table 3: IRIS spectrograph channels. Dispersion, Camera Electronics Box (CEB) and Effective Area (EA) vary for the three band passes

IRIS_Auto3

Figure 22: Spectrograph optical layout (image credit: NASA)

Many mechanical and electronic parts, drawings and designs are being re-used from the successful TRACE, Solar-B/Hinode, SECCHI and AIA/HMI programs. For example, the IRIS telescope, built at SAO (Smithsonian Astrophysical Observatory), Cambridge, MA, is based on the design of one of the AIA (Atmospheric Imaging Assembly) telescopes. The spectrograph is being built by MSU and LMSAL and NASA/ARC (Ames Research Center) will provide mission operations support.

The data handling and pipeline will be based on the existing AIA data pipeline, with Stanford University playing a major role in the operation of the data pipeline. Data will be downlinked through an X-band antenna at ground stations in Svalbard in Norway (funded by the Norwegian Space Center) and in Alaska and other NASA sites.

IRIS science investigation (Ref. 8):

The IRIS spectra will cover temperatures from 4,500 K to 10 MK, with the images covering temperatures from 4,500 K to 65,000 K. The CCD detectors will have 1/6 arc second pixels. IRIS will have an effective spatial resolution between 0.33 and 0.4 arcsec and a maximum field of view of 170 arcsec x 170 arcsec.

IRIS will have thermal coverage from the photosphere (neutral lines, wings of Mg II h/k) through the chromosphere (Mg II h/k) and transition region (C II, Si IV, O IV) into the corona (Fe XII and Fe XXI). This will allow the project to fully trace and identify the connections between all regions in the solar atmosphere. The high throughput of the instrument will allow short exposure times that enable measurements of the intensity, Doppler shift (down to 1 km/s), line width., and reconstruct images.

Deeper exposures will also reveal the full shape of the spectral line profiles (e.g., asymmetries). The short exposure times and flexible rastering schemes (Figure 23) will allow rapid scans of small regions on the Sun at very high spatial resolution of order 0.33-0.40 arcsec. IRIS will function as a microscope for instruments onboard Solar-B/Hinode and the SDO (Solar Dynamics Observatory), which have a spatial and temporal resolution that is significantly reduced compared to IRIS.

The sparse raster option will allow rapid scans of much larger areas, which can be used, for example, for flare or CME (Coronal Mass Ejection) watch programs (Figure 23). The simultaneous images will have broader spectral range, so they will contain a mixture of continuum and upper chromospheric (Mg II k) or transition region (C II, Si IV) emission. The upper chromospheric and transition region contributions are estimated to be in excess of 50% of the total emission of in these spectral regions.

IRIS_Auto2

Figure 23: High throughput allows for rapid rasters of high S/N spectra that enable line centroid velocity determination down to 1 km/s precision within 1 s exposures for the brightest lines (image credit: LMSAL)

IRIS will be operated in a manner that is similar to TRACE and Solar-B/Hinode, with observing programs uploaded 5 times per week, and the data made publicly available within a day of the observation. The project will operate IRIS in full coordination with Solar-B/Hinode and SDO. To augment the IRIS data, the project will have a special focus on coordination with ground-based observations that obtain chromospheric spectral line profiles over a large field of view (using Fabry-Perot interferometers). The Mg II h/k lines are optically thick lines, so require careful analysis for a proper interpretation. This can be done using 3D radiative MHD (Magneto-Hydrodynamic) models and non-LTE radiative transfer diagnostic software tools such as MULTI and RH. This approach is essential because of the highly dynamic and rapidly spatially varying nature the chromosphere.

In summary, the IRIS science investigation will focus on combining IRIS data with Solar-B/Hinode, SDO and ground-based observations, together with numerical MHD and multi-fluid plasma simulations to develop a comprehensive picture of the flow of energy and mass in the solar atmosphere. Given the complexity of the interface region, the interplay between observations and simulations will be very important. The IRIS science investigation has a strong theory/numerical modeling component. State-of-the-art radiative 3D MHD numerical simulations and synthetic (non-LTE) diagnostics in, e.g., optically thick lines like Mg II h/k, will allow creation of simulated data for detailed comparisons with IRIS observations (Ref. 8).

IRIS_Auto1

Figure 24: Photo of the IRIS telescope (image credit: NASA)

 


 

Ground segment:

The MOS (Mission Operations System) and GDS (Ground Data System) were developed by NASA/ARC (Ames Research Center). The MMOC (Multi-Mission Operations Center) is housed and staffed by NASA Ames personnel. The GDS is supported by NASA's NEN (Near-Earth Network) and the NSC (Norwegian Space Center) with ground stations in Svalbard, Alaska, and Wallops Island. The observatory operates autonomously with one command pass during nominal working days (5 days per week). Science team members prepare observation timelines that include pointing targets, scans and slews, and coordinated observation sequences with other missions and observatories. The timelines are prepared the day prior to the command load and cover weekends and holidays (Ref. 10).

The science data is downlinked via 13 ground station passes per day (7 days per week). The MOC is staffed for the command passes with lights out operation the remainder of the time. The data from each ground station pass is transferred autonomously using standard internet protocol. The observatory has a fault management system that monitors subsystem telemetry points and determines if immediate action is required or if alerts are to be sent to the ground. The team has a health and safety web page viewable by all team members and an Alert Notification System on the ground that monitors telemetry and sends out text messages if any program parameters go out of range. IRIS generates more than 45 Gb of science data/day. The data is transferred from the NASA MMOC to the SDO (Solar Dynamics Observatory) Science Operations Center at Stanford, where preliminary processing is performed. The quicklook data is typically available on an open access basis to the science community within 6 hours of receipt on the ground. Calibrated data is available 7 days after receipt on the ground.

IRIS_Auto0

Figure 25: IRIS mission concept (image credit: LMSAL)

Throughout design, development, integration, and test, the instrument, spacecraft, MOS/GDS, and science teams were integrated and co-located as much as possible. Many personnel who worked on the instrument and spacecraft subsystems and components were part of the program from design phase to launch and on-orbit checkout. This was an important part of the program as it ensured: continuity of knowledge from design to test, that subsystem test scripts could be modified and carried into observatory test, and that anomaly and root cause investigations could be carried out in a timely manner. This also enabled team members to cross-train on other subsystems allowing the relatively small team to carry out the environmental, comprehensive and functional tests, launch operations, and on-orbit checkout and calibration.

A common ground system EGSE operating system, ITOS (Integrated Test and Operations System), was selected for the instrument, spacecraft, and mission operations systems. This allowed test scripts and display screens developed during subassembly integration and test to be migrated to the system level testing and to the MOC. EGSE imaging and analysis routines from AIA and HMI were ported for use on IRIS. The spacecraft EGSE was developed for the IRIS program with a few components such as the Solar Array Simulators and RF test equipment made available from prior programs. The optical stimulus GSE – used for performance testing of the instrument throughout integration and test - was based on the AIA stimulus system including use of a spare telescope tube. In addition, a set of company processes and procedures were tailored to meet the scope and pace of the mission.

 


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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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