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Propellant injection systems and processesThe previous 'Art of Injector Design' is maturing and merging with the more systematic 'Science of Combustion Device Analysis.' This technology can be based upon observation, correlation, experimentation and ultimately analytical modeling based upon basic engineering principles. This methodology is more systematic and far superior to the historical injector design process of 'Trial and Error' or blindly 'Copying Past Successes.' The benefit of such an approach is to be able to rank candidate design concepts for relative probability of success or technical risk in all the important combustion device design requirements and combustion process development risk categories before committing to an engine development program. Even if a single analytical design concept cannot be developed to predict satisfying all requirements simultaneously, a series of risk mitigation key enabling technologies can be identified for early resolution. Lower cost subscale or laboratory experimentation to demonstrate proof of principle, critical instrumentation requirements, and design discriminating test plans can be developed based on the physical insight provided by these analyses.
Document ID
19950020361
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Ito, Jackson I.
(GenCorp Aerojet Sacramento, CA, United States)
Date Acquired
September 6, 2013
Publication Date
January 1, 1995
Subject Category
Propellants And Fuels
Report/Patent Number
NAS 1.15:110632
NASA-TM-110632
Report Number: NAS 1.15:110632
Report Number: NASA-TM-110632
Meeting Information
Meeting: International Symposium on Liquid Rocket Propulsion
Location: Paris
Country: France
Start Date: June 19, 1995
End Date: June 21, 1995
Accession Number
95N26781
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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