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High performance N204/amine elements: BlowapartThe work is reported which was conducted to define the mechanisms governing blowapart of hypergolic propellant through the design, fabrication, test, and analysis of single element injectors. Data were developed that show the parameters exhibiting a controlling influence over blowapart are the chamber pressure, orifice diameter, and propellant temperature. Mixing, popping (cyclic blowapart), low pressure separation, and high pressure separation were identified as modes of reactive impingement.
Document ID
19750022253
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
November 15, 1974
Subject Category
Propellants And Fuels
Report/Patent Number
REPT-14186-DRL-3-1
NASA-CR-141480
Report Number: REPT-14186-DRL-3-1
Report Number: NASA-CR-141480
Accession Number
75N30326
Funding Number(s)
CONTRACT_GRANT: NAS9-14186
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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