The scientific objective of the Spartan 201 or Solar Spartan (Shuttle Pointed Autonomous Research Tool
for Astronomy) mission is to probe the physics of solar-wind acceleration by observing the
hydrogen, proton and electron temperatures and densities, and the solar-wind velocities in
a variety of coronal structures at locations from 1.5 to 3.5 solar radii from the Sun. The
instruments are an ultraviolet coronal spectrometer and a white-light coronagraph. The
spectrometer measures the intensities of Lyman alpha (1215 A) and the intensities of the
Oxygen VI lines (1031.9 and 1037.6 A). The white-light coronagraph measures the intensity
and polarization of the electron-scattered white-light corona. Both of these instruments
have been used in previous sounding rocket flights. The instruments are housed together in
a cylinder that is 0.43 m in diameter and 3 m long.
The Spartan program provides a series of low-cost, free-flying space platforms to
perform various scientific studies. A Spartan is launched aboard the Space Shuttle and
deployed from the Orbiter, where it performs a pre-programmed mission. Scientific data are
collected during each mission using a tape recorder and, in many cases, film cameras.
There is no command and control capability after deployment. The Spartan is then retrieved
by the Orbiter and returned to Earth for recovery of the data, refurbishment and
preparation for future missions. Power during the deployed phase of the mission is
provided by on-board batteries, and attitude control is accomplished with pneumatic gas
jets. The onboard tape recorder provides approximately 6E9 bits of storage capacity for
experiments.
This experiment was flown and retrieved five times.
