MicroNimbus is a small satellite mission being developed by the Georgia Institute of Technology and Georgia Tech Research Institute that will utilize a frequency-agile mm-wave radiometer to measure and update the temperature profile of the atmosphere from a 3U CubeSat platform. The on-board radiometer instrument will provide atmospheric temperature profile data at an altitude resolution of 10 km, a geographic resolution of 0.5°, and a temperature resolution of 2K RMS. The mission strongly aligns with the goals set forth in NASA’s Science Plan and will generate data valuable to researchers in the fields of weather forecasting, LIDAR, and laser communications.

MicroNimbus has passed its Preliminary Design Review (PDR) phase and is moving towards the Critical Design Review (CDR) for the mission. If successful, MicroNimbus will serve as a first step towards the creation of a constellation of satellites designed to perform near real-time temperature profiling of the atmosphere. Atmospheric sounding missions have played a critical role in NASA’s and NOAA’s ability to monitor, analyze, and predict weather over both short and long time scales. One example of this is the NASA Nimbus 6 satellite − part of the Nimbus series of missions (to which MicroNimbus’ name pays homage). One of the many instruments carried by Nimbus 6 was a passive microwave radiometer in the 60 GHz regime that was used to retrieve atmospheric temperature profiles. Another similar, and currently active, mission by NASA is the Aqua (EOS PM-1) satellite. Specifically, the AMSU instrument onboard Aqua is capable of scanning between 10 channels in the ∼60 GHz range where O2 absorption lines occur.

However, the need for global, near real-time weather and temperature measurements has led researchers to look into the use of small satellites, specifically CubeSats, to obtain this data. In recent years, CubeSats have been utilized by the scientific community in the area of remote sensing due to their low cost, fast development schedules, and unique mission architecture configurations (formations, constellations, etc.) MicroNimbus attempts to do just this; to perform scientific experiments similar to those carried out by Nimbus 6 and Aqua at a fraction of the cost and development time.

Specifically, the MicroNimbus mission attempts to miniaturize the design of a microwave radiometer, such as the Nimbus 6 SCAMSa and the AQUA’s AMSU instrument, through the use of a silicon-germanium (SiGe) integrated receiver front end and a corrugated horn antenna design. While SCAMS and AMSU focused on scanning three and ten different O2 absorption bands respectively, MicroNimbus will scan through seven. Furthermore, MicroNimbus will make use of the CubeSat platform in order to reduce the cost and development times required to obtain this type of atmospheric sounding data

Sources and Additional Information:

  1. https://ieeexplore.ieee.org/document/8127564
  2. https://apps.dtic.mil/dtic/tr/fulltext/u2/1076181.pdf
  3. https://arc.aiaa.org/doi/pdfplus/10.2514/6.2018-1941
  4. Parkinson, C. L., “Aqua: An Earth-observing satellite mission to examine water and other climate variables,” IEEE Transactions on Geoscience and Remote Sensing, Vol. 41, No. 2, 2003, pp. 173–183.
  5. Selva, D. and Krejci, D., “A survey and assessment of the capabilities of Cubesats for Earth observation,”
    Acta Astronautica, Vol. 74, 2012, pp. 50–68.
Full NameMicroNimbus
Launch Date
Downlink Frequency

Space Missile Defense Command – Technology Satellite

TechSat is a satellite produced through the US Army and the Department of Defense.

Craft Overview:

TechSat was designed to combine two key pieces of technology into one spacecraft: high power architecture with articulated solar arrays and a commercial off-the-shelf (COTS) high performance parallel processing computer.

Sources and Additional Information:

  1. J. R. Samson, “Small, light-weight, low-power, low-cost, high performance computing for CubeSats,” 2014 IEEE Aerospace Conference, 2014, pp. 1-10, doi: 10.1109/AERO.2014.6836523.
  2. https://space.skyrocket.de/doc_sdat/smdc-techsat.htm
AcronymSMDC TechSat
Full NameSpace Missile Defense Command – Technology Satellite
Launch Datecirca 2012
Principal InvestigatorBrian Gunter

ISS Airlock Handrail Antenna

The ISS Orlan antenna designed and built at Georgia Tech Research Institute offered a unique new form for antennas.  The 2 ft towel shaped antenna doubles as a handrail and allows for communication between suited astronauts within the airlock and the rest of the crew on board.  The ISS Orlan antenna was especially designed to work with Russian spacesuits, which at the time of launch operated on an unusual frequency that barely resonated within the airlock and contained no antennas of their own. The ISS Orlan antenna can also withstand huge temperature swings and forces experienced when space packs hit it.

Craft Overview:

The 2 ft towel bar antenna was built using a special “loop” design that couples a sufficient amount of RF energy tot he astronaut, instead of reflecting the energy off the walls of the airlock.


The ISS Orlan antenna launched as part of the STS-104 mission, where Shuttle Atlantis delivered the completed airlock to the ISS in July of 2001.

Sources and Additional Information:

  1. https://smartech.gatech.edu/bitstream/handle/1853/8758/40%20Departments.pdf?sequence=1&isAllowed=y
  2. https://ieeexplore.ieee.org/stamp/stamp.jsp?arnumber=883504
  3. https://www.militaryaerospace.com/home/article/16707591/georgia-tech-develops-space-antenna
NameISS Orlan Antenna/ISS Airlock Handrail Antenna
Size2 ft
Launch DateJuly 2001
Principal InvestigatorVictor Tripp