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Hydrazine engine plume contamination mappingInstrumentation for the measurement of plume exhaust specie deposition rates were developed and demonstrated. The instruments, two sets of quartz crystal microbalances, were designed for low temperature operation in the back flow and variable temperature operation in the core flow regions of an exhaust plume. These quartz crystal microbalances performed nominally, and measurements of exhaust specie deposition rates for 8400 number of pulses for a 0.1-lb monopropellant thruster are reported.
Document ID
19760018257
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Chirivella, J. E.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Date Acquired
September 3, 2013
Publication Date
October 1, 1975
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
NASA-CR-147936
AD-A018729
AFRPL-TR-75-16
Report Number: NASA-CR-147936
Report Number: AD-A018729
Report Number: AFRPL-TR-75-16
Accession Number
76N25345
Funding Number(s)
CONTRACT_GRANT: NAS7-100
PROJECT: AF PROJ. 5730
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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