XSS-10 computer model
|Launch mass||28 kilograms (62 lb)|
|Start of mission|
|Launch date||January 29, 2003, 18:06:00UTC|
|Rocket||Delta II 7925-9.5|
|Launch site||Cape Canaveral SLC-17B|
|Perigee||518.0 kilometers (321.9 mi)|
|Apogee||805.0 kilometers (500.2 mi)|
|Epoch||29 January 2003, 13:06:00 UTC|
XSS-10 (eXperimental Small Satellite 10) was a small, low-cost micro-spacecraft developed by the U.S. Air Force Research Laboratory’s Space Vehicles Directorate to test technology for line-of-sight guidance of spacecraft. The project was initiated at AFRL by Program Manager David Barnhart  and completed by Georgia Tech Research Institute engineer Thom Davis and team. The project was declared a success shortly after launch.
- "NASA - NSSDCA - Spacecraft - Trajectory Details". nssdc.gsfc.nasa.gov. Retrieved 2018-05-02.
- Banke, Jim (2003-01-30). "Air Force XSS-10 Micro-Satellite Mission a Success". Space.com. Archived from the original on May 13, 2008. Retrieved 2008-07-28.
- David A. Barnhart et al, “XSS-10 Micro-satellite Demonstration,” AIAA-1998-5298, AIAA Defense and Civil Space Programs Conference and Exhibit, Huntsville, AL, Oct. 28-30, 1998
- "Big plans for small satellites". Historical archive. Georgia Tech Research Institute. Retrieved 2012-10-26.
- Sanders, Jane M (2003-08-11). "The Little Engine That Could". Research Horizons. Georgia Institute of Technology. Retrieved 2012-10-26.
- XSS Micro-Satellite at Boeing.com
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