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Space Shuttle contamination overviewConsideration is given to particle and gaseous contamination associated with Shuttle payload orbital delivery. An approach to control contamination is discussed which consists of analytical environment assessment, vehicle design optimization, and flight environment measurement. The analytical assessment of orbital contamination source characteristics and their effects on the Shuttle orbital environment has resulted in vehicle design changes and a detailed understanding of system operational flexibility. Verification of resulting Shuttle contamination performance will be made by the Induced Environment Contamination Monitor.
Document ID
19790033645
Acquisition Source
Legacy CDMS
Document Type
Conference Proceedings
Authors
Leger, L.
(NASA Lyndon B. Johnson Space Center Houston, TX, United States)
Jacobs, S.
(NASA Lyndon B. Johnson Space Center Houston, TX, United States)
Ehlers, H. K. F.
(NASA Johnson Space Center Houston, Tex., United States)
Date Acquired
August 9, 2013
Publication Date
January 1, 1978
Subject Category
Spacecraft Design, Testing And Performance
Meeting Information
Meeting: In: Aerospace Testing Seminar
Location: Los Angeles, CA
Start Date: March 2, 1978
End Date: March 3, 1978
Accession Number
79A17658
Distribution Limits
Public
Copyright
Other

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