MinXSS Flight Model 1.jpg
The sun-facing side of the MinXSS spacecraft. The two hinged solar panels are in their deployed state. The science instrument apertures can be see near the top. The tape-measure antenna extends beyond the top of the photo. Image taken after final integration of the spacecraft.
Mission typeSolar physics, Space weather, Near space research
COSPAR ID1998-067HU Edit this at Wikidata
SATCAT no.41474U
Mission durationFlight model 1: 6 months (planned), 11.66 months (actual)
Flight model 2: 5 years (planned)
Spacecraft properties
Spacecraft type3U CubeSat
Launch mass3.5163 kg
Dry mass3.5163 kg
8.0 W (science mode)
5.3 W (safe mode)
2.8 W (phoenix mode)
Max generation: 19 W
Start of mission
Launch dateDecember 6, 2015, 08:44:57 (2015-12-06UTC08:44:57Z) UTC
RocketAtlas V 401
Launch siteKennedy Space Center
ContractorUnited Launch Alliance
Entered service2016 May 16
End of mission
Last contact2017-05-06 02:37:26 UTC
Decay date2017 May 6
Orbital parameters
Reference systemGeocentric
RegimeLow Earth
Perigee altitude402 kilometers (250 mi)
Apogee altitude402 kilometers (250 mi)
Inclination51.65 degrees
Period92.69 minutes
EpochJuly 4, 2016[1]
Modified Amptek X123 silicon drift detector
Sun Position Sensor (SPS), X-ray Photometer (XP)

The Miniature X-ray Solar Spectrometer (MinXSS) CubeSat was the first launched National Aeronautics and Space Administration Science Mission Directorate CubeSat with a science mission.[2] It was designed, built, and operated primarily by students at the University of Colorado Boulder with professional mentorship and involvement from professors, scientists, and engineers in the Aerospace Engineering Sciences department and the Laboratory for Atmospheric and Space Physics, as well as Southwest Research Institute, NASA Goddard Space Flight Center, and the National Center for Atmospheric Research's High Altitude Observatory. The mission principal investigator is Dr. Thomas N. Woods and co-investigators are Dr. Amir Caspi, Dr. Phil Chamberlin, Dr. Andrew Jones, Rick Kohnert, Professor Xinlin Li, Professor Scott Palo, and Dr. Stanley Solomon. The student lead (project manager, systems engineer) was Dr. James Paul Mason, who has since become a Co-I for the second flight model of MinXSS.

MinXSS launched on 2015 December 6 to the International Space Station as part of the Orbital ATK Cygnus CRS OA-4 cargo resupply mission.[3] The launch vehicle was a United Launch Alliance Atlas V rocket in the 401 configuration. CubeSat ridesharing was organized as part of NASA ELaNa-IX. Deployment from the International Space Station was achieved with a NanoRacks CubeSat Deployer on 2016 May 16.[4] Spacecraft beacons were picked up soon after by amateur radio operators around the world.[5][6] Commissioning of the spacecraft was completed on 2016 June 14[7] and observations of solar flares captured nearly continuously since then.[8] The altitude rapidly decayed in the last week of the mission as atmospheric drag increased exponentially with altitude. The last contact from MinXSS came on 2017-05-06 at 02:37:26 UTC from a HAM operator in Australia. At that time, some temperatures on the spacecraft were already in excess of 100 °C. (One temperature of >300 °C indicated that the solar panel had disconnected, suggesting this contact was only moments before disintegration.)[9] Science data spanning the entire mission are publicly available.[10]

Mission objective

The MinXSS mission is to measure the solar soft X-ray spectrum from about 0.5 keV (25 Å) to 30 keV (0.4 Å) with ~0.15 keV FWHM spectral resolution. This part of the solar electromagnetic spectrum is where the largest enhancement from solar flares is expected to occur.[11] It also has an important impact on Earth ionospheric chemistry. Despite this, prior measurements have been either low-resolution broadband, or high-resolution but very narrow bandpass (see image below).[12][13] The relatively recent creation of miniaturized silicon drift detectors has enabled the MinXSS measurements. MinXSS data will provide a means of probing the solar corona—especially in active regions and solar flares—and will be used as an input for models of the Earth's upper atmosphere, particularly the ionosphere, thermosphere, and mesosphere.

Solar soft X-ray measurement history
Solar soft X-ray measurement history

MinXSS is also the first flight of the Blue Canyon Technologies XACT attitude determination and control system (ADCS), one of the only commercially available 3-axis ADCSs for CubeSats. It is performing even better than its specification.[14] This demonstrates that a critical technology for spacecraft has been successfully miniaturized and commercialized.

Science instrument

The primary science instrument onboard MinXSS is a modified Amptek X123 silicon drift detector. The instrument was modified to make it compatible with a space environment.[13] Specifically, heat transfer pads were placed on the hottest components of the electronics boards to provide a conductive thermal path for heat transfer. In atmosphere, the electronics can cool convectively, but operation in vacuum requires cooling via conduction and hence an improved conductive path. Additionally, a small aperture made of tungsten was attached to the front of the detector to reduce the likelihood of photon saturation and limit the field of view to ±4º. Finally, an additional beryllium filter was mounted in front of the detector to reduce the number of photoelectrons reaching the detector.

There are two secondary science instruments: the X-ray Photometer (XP) and the Sun Position Sensor (SPS). XP is a single photodiode with a beryllium filter in front of it of nearly identical thickness to the sum of the two beryllium filters in front of the X123. The purpose of XP is provide an on-orbit cross-calibration for the X123: the sum of the X123 spectrum should be approximately equal to the XP measurement. SPS is a fine sun sensor with 2.4 arcsec precision that consists of a planar quad-diode observing visible light, whose purpose is to provide fine knowledge of the solar position with respect to the X123 and XP optical axes to correct for any off-axis signal attenuation.

All instruments were calibrated at the National Institute of Standards and Technology's Synchrotron Ultraviolet Radiation Facility (SURF III).[12][15]

Pre-flight testing

Despite the loose requirements placed on CubeSats compared to larger spacecraft missions, MinXSS underwent the same rigorous tests that are considered standard in the aerospace industry. The X123 primary science instrument was fully flight-qualified on two sounding rocket flights.[12][16] In addition to subsystem-level and system-level testing at the bench (i.e. in air at room temperature), the system also underwent thermal vacuum chamber cycle testing, thermal balance testing, vibration testing, and end-to-end communications testing.[13] Mission simulations were performed during thermal vacuum cycling and at the bench using a solar array simulator that was autonomously power toggled with realistic orbital insolation and eclipse periods. This ensured that the spacecraft would be power-positive on orbit.


The spacecraft uses a measuring tape antenna and an AstroDev Li-1 radio. The spacecraft periodically beacons and its signal can be picked up with amateur ham radio operator equipment. Below are the communications specifications:[17]

Beacons recorded by ham radio operators can be sent to the MinXSS team (in KISS format) to contribute to overall data capture.[17]

On-Orbit success

The first critical hurdle for any deployed spacecraft is to establish communications with the ground. This was achieved on the first pass over the MinXSS ground station in Boulder, Colorado.[18] As a science mission, success is determined by receipt of useful scientific measurements. MinXSS first light was presented at a press briefing and a contributed poster during the American Astronomical Society's 47th Solar Physics Division Meeting in Boulder, Colorado.[19][20][21] Over 40 GOES C-class and 7 M-class solar flares occurred in the first weeks of the MinXSS mission, and those observations were downlinked to the ground for analysis. The results of those analyses will be the subjects of several upcoming peer-review papers. Additionally, MinXSS was the first flight of the Blue Canyon Technologies XACT 3-axis attitude determination and control system (ADCS). It continuously performed exceptionally, with 8 arcsecond (1-sigma) pointing, where the specification was for 11 arcseconds.[14]

Follow-on mission (MinXSS-2)

A second MinXSS spacecraft was built in parallel with the first. MinXSS-2 is identical to MinXSS-1 except for:

MinXSS-2 is planned to deploy from the Spaceflight Industries SSO-A SmallSat Express mission,[22] using a SpaceX Falcon 9.[23] Launch happened on 3 December 2018, and MinXSS2 was deployed to orbit. The MinXSS-2 orbit is polar and sun-synchronous at 10:30am LTDN, at approximately 575 km altitude, providing an estimated 4-year mission life.

MinXSS-2 was selected for 2 years of funding by NASA under the 2016 Heliophysics Technology and Instrument Development for Science (H-TIDeS) program.[24] MinXSS-2 also adds science involvement from the Naval Research Laboratory, with Dr. Harry Warren added as a co-investigator.


MinXSS was chosen as the 2016 AIAA Small Satellite Mission of the Year during the 30th Annual AIAA/USU Small Satellite Conference in Logan, UT.[25][26]

Project architecture

The MinXSS project was structured after the Colorado Student Space Weather Experiment CubeSat, which established the graduate projects course led by Joseph R. Tanner in the Aerospace Engineering Sciences department at the University of Colorado Boulder. Students in the department have the choice to either complete a Master's thesis or take two semesters of the graduate projects course. Typically, 10-20 students will be involved in each of the concurrent projects. CSSWE and MinXSS heavily leveraged professionals at the Laboratory for Atmospheric and Space Physics. As of 2018 March 8, 40 graduate, 5 undergraduate, and two high school students have worked on the project. Roughly 40 professionals have contributed with varying levels of involvement, from providing feedback at design reviews to writing flight software.


  1. ^ Celestrak NORAD CubeSat TLEs
  2. ^ "Achieving Science with CubeSats: Thinking Inside the Box". NationalAcademies.org. Retrieved 9 August 2016.
  3. ^ "MinXSS CubeSat Launches to ISS to Study Sun's Soft X-Rays". NASA.gov. Retrieved 9 August 2016.
  4. ^ "MinXSS CubeSat Deployed From ISS to Study Sun's Soft X-Rays". NASA.gov. Retrieved 9 August 2016.
  5. ^ "MinXSS 20:26 UTC 437.345mhz 9K6 Telemetry interval 9 seconds over Japan strong signal". Twitter. Retrieved 9 August 2016.
  6. ^ "MINXSS and NODeS 02:57 UTC May 17 2016". YC3BVG BLOG. Retrieved 9 August 2016.
  7. ^ "Commissioning complete!". MinXSS Homepage. Retrieved 9 August 2016.
  8. ^ "MinXSS CubeSat Deployed From ISS to Study Sun's Soft X-Rays". NASA.gov. Retrieved 7 October 2016.
  9. ^ "The Miniature X-ray Solar Spectrometer (MinXSS) » MinXSS-1 deorbited". lasp.colorado.edu. Retrieved 2017-05-08.
  10. ^ "The Miniature X-ray Solar Spectrometer (MinXSS) » Data and HAM Radio". lasp.colorado.edu. Retrieved 2017-05-08.
  11. ^ Rodgers, E. M.; Bailey, S. M.; Warren, H. P.; Woods, T. N.; Eparvier, F. G. (9 September 2006). "Soft X-ray irradiances during solar flares observed by TIMED-SEE". Journal of Geophysical Research: Space Physics. 111 (A10): A10S13. Bibcode:2006JGRA..11110S13R. doi:10.1029/2005JA011505.
  12. ^ a b c Caspi, Amir; Woods, Thomas N.; Warren, Harry P. (18 March 2015). "New Observations of the Solar 0.5-5 keV Soft X-ray Spectrum". Astrophysical Journal Letters. 802 (1): L2. arXiv:1502.01725. Bibcode:2015ApJ...802L...2C. doi:10.1088/2041-8205/802/1/L2.
  13. ^ a b c Mason, James P.; Woods, Thomas N.; Caspi, Amir; Chamberlin, Phillip C.; Moore, Christopher; Jones, Andrew; Kohnert, Rick; Li, Xinlin; Palo, Scott; Solomon, Stanley C. (10 March 2016). "Miniature X-Ray Solar Spectrometer: A Science-Oriented, University 3U CubeSat". Journal of Spacecraft and Rockets. 53 (2): 328–339. arXiv:1508.05354. Bibcode:2016JSpRo..53..328M. doi:10.2514/1.A33351.
  14. ^ a b "Perfect Precision For MinXSS CubeSat Supplied By Blue Canyon Technologies—It's All About Attitude". Satnews. Retrieved 9 August 2016.
  15. ^ Moore, Christopher S.; Woods, Thomas N.; Caspi, Amir; Mason, James P. (18 July 2016). "The Miniature X-ray Solar Spectrometer (MinXSS) CubeSats: spectrometer characterization techniques, spectrometer capabilities, and solar science objectives". Proc. SPIE. Space Telescopes and Instrumentation 2016: Ultraviolet to Gamma Ray. 9905: 990509. arXiv:1608.05115. Bibcode:2016SPIE.9905E..09M. doi:10.1117/12.2231945. Retrieved 9 August 2016.
  16. ^ "NASA-Funded Mission Studies the Sun in Soft X-Rays". NASA.gov. Retrieved 9 August 2016.
  17. ^ a b "Data & Ham Radio". MinXSS Homepage. Archived from the original on 21 August 2016. Retrieved 9 August 2016.
  18. ^ "First day on orbit a great success!". MinXSS Homepage. Retrieved 9 August 2016.
  19. ^ Kohler, Susanna. "2016 SPD: Day 1". AASNova. Retrieved 9 August 2016.
  20. ^ Patel, Neel V. "4 Technologies NASA Is Using to Save Us From Death by Sun". Inverse. Retrieved 9 August 2016.
  21. ^ Caspi, Amir; Woods, Thomas N.; Warren, Harry P.; Chamberlin, Phillip C.; Jones, Andrew; Mason, James P.; McTiernan, James M.; Moore, Christopher S.; Palo, Scott E.; Solomon, Stanley C. (31 May 2016). "Science Goals and First Light Analysis from the Miniature X-ray Solar Spectrometer (MinXSS) CubeSat". American Astronomical Society, SPD Meeting #47: #3.06. Bibcode:2016SPD....47.0306C. Retrieved 9 August 2016.
  22. ^ "Spaceflight Prepares Historic Launch of More Than 70 Spacecraft Aboard SpaceX Falcon 9". spaceflight.com. Retrieved 10 September 2018.
  23. ^ "Spaceflight gears up for dedicated Falcon 9 launch". SpaceNews. Retrieved 10 September 2018.
  24. ^ "MinXSS-2 has been selected by NASA for funding!". Twitter. Retrieved 11 December 2016.
  25. ^ "MinXSS is the @SmallSat mission of the year!Thanks all who voted and made such an exciting and successful mission". Twitter. Retrieved 11 August 2016.
  26. ^ "MinXSS wins Mission of the Year at Small Sat Conference". CU Aerospace Engineering Sciences. Retrieved 26 August 2016.