XSS-10
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Mission type | Technology |
---|---|
Operator | AFRL |
COSPAR ID | 2003-005B |
SATCAT no. | 27664 |
Spacecraft properties | |
Manufacturer | Boeing |
Launch mass | 28 kilograms (62 lb) |
Start of mission | |
Launch date | January 29, 2003, 18:06:00 | UTC
Rocket | Delta II 7925-9.5 (Delta 295) |
Launch site | Cape Canaveral SLC-17B |
Orbital parameters | |
Reference system | Geocentric |
Regime | Low Earth |
Eccentricity | 0.020384971 |
Perigee altitude | 518.0 kilometers (321.9 mi) |
Apogee altitude | 805.0 kilometers (500.2 mi) |
Inclination | 39.75 degrees |
Period | 98.0 minutes |
Epoch | 29 January 2003, 13:06:00 UTC[1] |
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.[2] The project was initiated at AFRL by Program Manager David Barnhart[3] and completed by Georgia Tech Research Institute engineer Thom Davis and team.[4] The project was declared a success shortly after launch.[5]
References
[edit]- ^ "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.
- ^ Barnhart, David A.; Hunter, Roger C.; Weston, Alan R.; Chioma, Vincent J.; Steiner, Mark; Larsen, William (October 1998). XSS-10 micro-satellite demonstration. AIAA Defense and Civil Space Programs Conference and Exhibit. Huntsville, AL: American Institute of Aeronautics and Astronautics. doi:10.2514/6.1998-5298. AIAA 1998-5298.
- ^ "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.
External links
[edit]- XSS Micro-Satellite at Boeing.com