USA 102
Also called Darpasat
General
| Designation | 23031 / 94017B |
| Launch date | 13 Mar 1994 |
| Country of origin | United States |
| Mission | Military: technology |
| Perigee/Apogee | 550/550 km ? |
| Inclination | 105° ? |
| Period | 95.9 min ? |
| Launch vehicle | Taurus 01 |
Operated by DARPA
End of life
| Decay | May 2002 |
External resources
sat-index articles
Technical data
Specifications
| Prime contractor | Ball Aerospace |
| Platform | |
| Mass at launch | 198 kg |
| Mass in orbit | |
| Dimension | |
| Solar array | |
| Stabilization | |
| DC power | |
| Design lifetime | 3 years |
Demonstrated new technologies, including a GPS receiver
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V0.144 - Converted on Sun, 03 Mar 2024 18:29:57 GMT - Updated quarterly
V0.144 - Converted on Sun, 03 Mar 2024 18:29:57 GMT - Updated quarterly