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Aerophysical plasma alleviationReentry plasma sheath alleviation by injecting sulfur hexafluoride or hydrazine into boundary layer
Document ID
19710011655
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Parmentier, E. M. (Avco-Everett Research Lab. MA, United States)
Weiss, R. F. (Avco-Everett Research Lab. MA, United States)
Wray, K. L. (Avco-Everett Research Lab. MA, United States)
Date Acquired
August 6, 2013
Publication Date
January 1, 1970
Publication Information
Publication: NASA. LANGLEY RES. CENTER THE ENTRY PLASMA SHEATH AND ITS EFFECTS ON SPACE VEHICLE ELECTROMAGNETIC SYSTEMS, VOL. 1 1970
Subject Category
Physics, Plasma
Accession Number
71N21130
Funding Number(s)
CONTRACT_GRANT: F04701-70-C-0128
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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