Solwind (P78-1)

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:

  • a gamma-ray spectrometer and particle detectors,
  • a white-light coronagraph and an extreme-ultraviolet heliograph,
  • a solar X-ray spectrometer and spectroheliograph,
  • an extreme-ultraviolet spectrometer,
  • a high-latitude particle spectrometer,
  • an X-ray monitor, and
  • a preliminary aerosol monitor

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
Further STP missions: