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Test program to demonstrate the stability of hydrazine in propellant tanksA 24-month coupon test program to evaluate the decomposition of propellant tanks is reported. The propellant fuel evaluated was monopropellant-grade hydrazine (N2H4), which is normally a colorless, fuming, corrosive, strongly reducing liquid. The degree of hydrazine decomposition was determined by means of chemical analyses of the liquid and evolved gases at the end of the test program. The experimental rates of hydrazine decomposition were determined to be within acceptable limits. The propellant tank materials and material combinations were not degraded by a 2-year exposure to hydrazine propellant. This was verified using change-of-weight determinations and microscopic examination of the specimen surface before and after exposure, and by posttest chemical analyses of hydrazine liquid for residual metal content.
Document ID
19830019985
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Moran, C. M.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Bjorklund, R. A.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Date Acquired
September 4, 2013
Publication Date
April 1, 1983
Subject Category
Propellants And Fuels
Report/Patent Number
NASA-CR-172768
NAS 1.26:172768
JPL-PUB-83-37
Accession Number
83N28256
Funding Number(s)
CONTRACT_GRANT: NAS7-100
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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