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The OSS-1/STS-3 missionIntegration, test, flight operations, program and science management, and experiment results from the OSS-1/STS-3 flight are reviewed. The experimental pallet, manufactured by ESA members, carried instrumentation for astronomy, space plasma studies, physics, planetology, solar physics, and life sciences. The ability of the equipment to operate in a worst-case Orbiter thermal environment was tested, as was the plasma environment around the Orbiter. The solar UV spectral irradiance monitor microprocessor was found to reset concurrently with start-up of the Shuttle hydraulic pumps. Degradations were also observed in one of the three solar flare X ray polarimeter modules, the thermal cannister experiment microprocessor, and the scientific data recorder no. 2. The Orbiter was determined to perform well during firing of an electron beam. A contamination monitor recorded matter accretion to be dependent on the solar orientation of the Orbiter. Finally, the distribution of the responsibilities and tasks for mission management are reviewed.
Document ID
19820064482
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Kissin, K.
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Eiband, M.
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Date Acquired
August 10, 2013
Publication Date
October 1, 1982
Subject Category
Space Transportation
Report/Patent Number
AIAA PAPER 82-1800
Report Number: AIAA PAPER 82-1800
Meeting Information
Meeting: Space Systems Conference: The Space Transportation System: A Review of Its Present Capability and Probable Evolution
Location: Washington, DC
Start Date: October 18, 1982
End Date: October 20, 1982
Sponsors: AIAA, DGLR, AAS, and BIS,
Accession Number
82A48017
Distribution Limits
Public
Copyright
Other

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