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Voyager 0.2-lbf thruster valve assembly short pulse test reportThe short pulse width testing completed on the Voyager 0.2-lbf thruster value assemblies (T/VA's) and the disassembly and inspection of T/VA S/N 020 is reported. The purpose for performing the short pulse width testing on Voyager 0.2-lbf thruster valve assemblies (T/VA's) was to determine: (1) impulse bit versus electrical pulse width; (2) impulse bit variations versus electrical pulse width; and (3) whether the short pulses decrease thruster life.
Document ID
19850024872
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Johnson, D. R. (Rocket Research Corp. Redmond, WA, United States)
Date Acquired
September 5, 2013
Publication Date
April 29, 1985
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
NASA-CR-176121
RRC-85-R-999
NAS 1.26:176121
Accession Number
85N33185
Funding Number(s)
OTHER: JPL-957181
PROJECT: JPL PROJ. 9950-1141
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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