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High performance N2O4/amine elements blowapartAn experimental and analytical program was conducted to develop an understanding of the mechanisms controlling hypergolic propellant reactive stream separation (RSS). RSS is a combustion induced phenomenon that results in striation of hypergolic propellant oxidizer and fuel sprays fans. This reduced intraelement mixing can influence thrust chamber performance, heat transfer, and stability. The program and product were the development of design criteria for coping with RSS to allow the design of high performance, stable injectors.
Document ID
19790019152
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Lawver, B. R.
(Aerojet Liquid Rocket Co. Sacramento, CA, United States)
Date Acquired
September 3, 2013
Publication Date
March 1, 1979
Subject Category
Propellants And Fuels
Report/Patent Number
NASA-CR-160272
Report Number: NASA-CR-160272
Accession Number
79N27323
Funding Number(s)
CONTRACT_GRANT: NAS9-14186
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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