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Shuttle payload integration - Contamination aspectsAs part of the development of the Space Shuttle, a payload integration system has been established. This integration system or process encompasses several technical disciplines, one of which is concerned with the control of molecular and particulate contamination. Specific integration procedures and documentation have evolved that reflect the incorporation of payload/Space Transportation System contamination requirements and capabilities. Of the 38 payloads in the payload integration system currently, about 20% are considered sensitive to contamination in that special precautions must be taken to ensure that contamination from the Space Shuttle Orbiter does not impair payload function. Most of these payload requirements have been satisfied by the incorporation of controlled ground operations discipline and installation of a payload bay liner, which isolates the payload from the Orbiter systems. Some payloads, however, provide covers for sensitive payload instrumentation.
Document ID
19830032529
Acquisition Source
Legacy CDMS
Document Type
Conference Proceedings
Authors
Jacobs, S.
(NASA Lyndon B. Johnson Space Center Houston, TX, United States)
Leger, L. J.
(NASA Lyndon B. Johnson Space Center Houston, TX, United States)
Ehlers, H. K. F.
(NASA Johnson Space Center Materials Technology Branch, Houston, TX, United States)
Date Acquired
August 11, 2013
Publication Date
January 1, 1982
Subject Category
Space Transportation
Meeting Information
Meeting: Shuttle optical environment
Location: Washington, DC
Start Date: April 23, 1981
End Date: April 24, 1981
Accession Number
83A13747
Distribution Limits
Public
Copyright
Other

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