DSX (SSTE-4, SET-1) |
USA |
Int. spacecraft nº: |
US spacecraft nº: |
Launch data:
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| Prime manufacturer | Microsat Systems Inc. (MSI) ? Sierra Nevada Corp. |
| Platform | 2 SN-200 (Road Runner) busses |
| Operator | AFRL |
| Mass at launch | ~600 kg |
| Dry Mass | kg |
| Basic shape | |
| Dimension (m) | |
| Equipment | WPIx, SWx, SFx (SET-1) |
| Solar array | Deployable solar array |
| Stabilization | |
| Propulsion | |
| DC power | |
| Design lifetime | 6 month |
![]() Illustration of the DSX stowed spacecraft configuration (image credit: AFRL, SNC) |
| Ref.: #6, #7(JR767), #14, #27, #228 - update: 16.11.19 | Home |