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Hypersonic research engine project. Phase 2: Structures and cooling developmentThe flightweight components were adapted to form the basic engine assembly. The water cooled test adapters for use in wind tunnel tests were fabricated. Commercially available valves were selected for the coolant control system. The simplification of the temperature control concept and of the absence of weight and volume constraints made it possible to use these valves. Various calibration tests are also discussed.
Document ID
19720018061
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Jilly, L. F. (AiResearch Mfg. Co. Los Angeles, CA, United States)
Date Acquired
August 6, 2013
Publication Date
September 1, 1970
Subject Category
Propulsion Systems
Report/Patent Number
NASA-CR-112055
ITR-14
AP-70-6640
Report Number: NASA-CR-112055
Report Number: ITR-14
Report Number: AP-70-6640
Accession Number
72N25711
Funding Number(s)
CONTRACT_GRANT: NAS1-6666
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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