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Gas-Centered Swirl Coaxial Liquid Injector EvaluationsDevelopment of Liquid Rocket Engines is expensive. Extensive testing at large scales usually required. In order to verify engine lifetime, large number of tests required. Limited Resources available for development. Sub-scale cold-flow and hot-fire testing is extremely cost effective. Could be a necessary (but not sufficient) condition for long engine lifetime. Reduces overall costs and risk of large scale testing. Goal: Determine knowledge that can be gained from sub-scale cold-flow and hot-fire evaluations of LRE injectors. Determine relationships between cold-flow and hot-fire data.
Document ID
20050217144
Acquisition Source
Marshall Space Flight Center
Document Type
Conference Paper
Authors
Cohn, A. K.
(Air Force Research Lab. United States)
Strakey, P. A.
(Air Force Research Lab. United States)
Talley, D. G.
(Air Force Research Lab. United States)
Date Acquired
September 7, 2013
Publication Date
January 1, 2005
Publication Information
Publication: Fifth International Symposium on Liquid Space Propulsion
Subject Category
Spacecraft Propulsion And Power
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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