Consideration 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.
Space Shuttle contamination overview
In: Aerospace Testing Seminar ; 1978 ; Los Angeles, CA
1978-01-01
Sonstige
Keine Angabe
Englisch
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NTIS | 1974
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NTRS | 1974