MISSION_DESCRIPTION |
Mission Overview
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The Midcourse Space Experiment (MSX) mission began with the launch of
the spacecraft on April 24, 1996 into a ~900 km polar orbit for a
nominal 5 year mission. The MSX mission was divided into three
phases.
Phase 1, which ended on February 26, 1997 with the depletion of the
cryogen, was devoted almost exclusively to observations with the
infrared telescope, SPIRIT III.
Phase 2, lasting from cryogen depletion through September 1997,
emphasized astronomy and atmospheric measurements with the UVISI
(Ultraviolet/Visible Imaging and Spectrographic Imaging) sensors.
Phase 3 began in October 1997 when the SBV (Space Based Visible)
Camera became a contributing sensor to the US Space Surveillance
Network.
Instruments on MSX included an infrared imaging camera (SPIRIT III),
ultraviolet/visible imaging and spectrographic imaging sensors
(UVISI), a visible-wavelength camera (SBV), and a suite of
contamination detectors.
Further information about the MSX spacecraft and instruments may be
found in [MILLETAL1994]:
Mill, J.D., R.R. O'Niel, S. Price, G.J. Romick, O.M. Uy, and 5 other
authors, Midcourse Space Experiment: Introduction to the spacecraft,
instruments, and scientific objectives, Journal of Spacecraft and
Rockets 31, 900-907, 1994.
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MISSION_OBJECTIVES_SUMMARY |
Mission Objectives Overview
===========================
The principal goal of MSX was to collect phenomenology data
in support of ballistic missile defense objectives. Additional
objectives were to collect data in support of a variety of civilian
science objectives in earth and atmospheric remote sensing and
astronomy. A full set of experiments mapped the galactic plane,
the IRAS (Infrared Astronomical Satellite) gaps, the zodiacal
background, confused regions away from the galactic plane, deep
surveys of selected fields at high galactic latitudes, large
galaxies, asteroids, and comets.
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