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Parametric analysis for steady-state performance of attitude-control thrustersParametric analysis for steady state performance of attitude control thrustor
Document ID
19670008986
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Ferrera, J. D. (Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Mc Kown, P. M. (Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Date Acquired
August 3, 2013
Publication Date
December 31, 1966
Subject Category
Auxiliary Systems
Accession Number
67N18315
Distribution Limits
Public
Copyright
Public Use Permitted.
Keywords
THRUSTOR
STEADY STATE
ATTITUDE CONTROL
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