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Mass transport contamination studyA theoretical analysis was performed to determine the effects of outgassing and waste dumping on the contamination field around an orbiting spacecraft. The spacecraft was assumed to be spherical in shape with the mass flow emitting uniformly from the spherical surface at a constant rate and in a D'Lambertian spatial distribution. The outflow of gases were assumed to be neutrally charged and of a single species with a molecular weight characteristic of a composite of the actual species involved in the mass flow. The theoretical analysis showed that, for outgassing only, less than 1.5 percent of the outgas products will return to the Skylab spacecraft as a result of intermolecular collisions. When the total mass flow from the spacecraft, including waste dumps and reaction control motor firings, was considered, it was estimated that about 30 percent will return to the spacecraft.
Document ID
19730012148
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Robertson, S. J.
(Lockheed Missiles and Space Co. Huntsville, AL, United States)
Date Acquired
September 2, 2013
Publication Date
January 1, 1972
Subject Category
Space Vehicles
Report/Patent Number
NASA-CR-124131
HREC-6554-4
Report Number: NASA-CR-124131
Report Number: HREC-6554-4
Accession Number
73N20875
Funding Number(s)
CONTRACT_GRANT: NAS8-26554
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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