
Solwind (P78-1) [STP]
The Solwind (Solar Wind, P78-1) mission was designed to obtain scientific data from earth and sun-oriented experiments. The spacecraft was sun-oriented and had its spin axis perpendicular to both the orbital plane and the satellite-sun line. The instrumentation consisted of:
Solwind was destroyed as an ASAT target while still producing valuable results.
| Nation: | USA |
|---|---|
| Type / Application: | Experimental |
| Operator: | USAF STP (Space Test Program) |
| Contractors: | ? |
| Equipment: | ? |
| Configuration: | ? |
| Propulsion: | ? |
| Power: | |
| Lifetime: | |
| Mass: | 850 kg |
| Orbit: | 560 km × 600 km, 97.9 |
| Satellite | Date | LS | Launch Vehicle | Remarks | |
|---|---|---|---|---|---|
| Solwind (P78-1) | 24.02.1979 | Va SLC-3W | Atlas-F OIS |