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Design, development, and flight of a spacecraft charging sounding rocket payloadResults of the flight of the spacecraft charging sounding rocket payload are given. The payload was designed to create charging by the emission of both positive ions and electrons. The relationship between environmental parameters and changes in vehicle potential during periods of emission was also studied.
Document ID
19790015838
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Cohen, H. A. (Air Force Geophysics Lab. Hanscom AFB, MA, United States)
Sherman, C. (Air Force Geophysics Lab. Hanscom AFB, MA, United States)
Mullen, E. G. (Air Force Geophysics Lab. Hanscom AFB, MA, United States)
Huber, W. B. (Tri-Con Assoc., Inc. El Segundo, Calif., United States)
Masek, T. D. (Hughes Res. Labs. El Segundo, Calif., United States)
Sluder, R. B. (PhotoMetrics, Inc. Menlo Park, Calif., United States)
Mizera, P. F. (Aerospace Corp. Menlo Park, Calif., United States)
Schnauss, E. R. (Aerospace Corp.)
Adamo, R. C. (SRI Intern. Corp.)
Nanevicz, J. E. (SRI Intern. Corp.)
Date Acquired
August 9, 2013
Publication Date
January 1, 1979
Publication Information
Publication: NASA. Lewis Res. Center Spacecraft Charging Technol., 1978
Subject Category
Spacecraft Design, Testing And Performance
Accession Number
79N24009
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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IDRelationTitle19790015830Collected WorksSpacecraft Charging Technology, 1978
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