Official name SAMPEX
Alternative name SAMPEX
Cospar ID 1992-038A
Norad ID 22012
Launch date 1992-07-03
Launch site AFWTR
Launch vehicle Scout-G1
Country/Organization USA
Type application Research, magnetosphere
Operator NASA
RCS size MEDIUM
Decay date 2012-11-13
Shape Hex Poly + 2 Pan
Mass (kg) 156.59
Height (m) 1.5
Width (m) 0.9
Depth (m) 1.5
Span (m^2) 1.5
Lifetime 3 years (design)
Contractors NASA Goddard Space Flight Center
Equipment HILT, LEICA, MAST, PET
Propulsion ?
Configuration Box, 2 solar panels, 3-axis control
Power 2 deployable fixed solar arrays, batteries

The main objectives of SAMPEX (Solar Anomalous & Magnetospheric Particle Explorer) experiments was to obtain data for several continuous years on the anomalous, components of cosmic rays, on energetic particle emissions from the sun, and on the precipitating magnetospheric relativistic electrons. It carries four instruments:

  • HILT (Heavy Ion Large Area Proportional Counter Telescope),
  • LEICA (Low Energy Ion Composition Analyzer),
  • MAST (Mass Spectrometer Telescope),
  • PET (Proton/Electron Telescope)

The spacecraft uses an on-board 3-axis stabilized solar pointed/momentum bias system, with the pitch axis pointed to the sun. Solar panels provide the power for the operations, including 16.7 W for the science instruments. The estimated useful lifetime of the spacecraft is about three years. An on-board DPU preprocesses the science and other data and stores them in a RPP unit of about 65 Mb, before transmitting in the S-band at a rate of 1.5 Mb/s over Wallops (or a back-up) station. The command memory can store at least a thousand commands.

Satellite COSPAR Date LS Launch Vehicle Remarks
SAMPEX 1992-038A 1992-07-03 AFWTR Scout-G1