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Hypersonic research engine project. Phase 2: Structures and cooling developmentThe structures assembly model (SAM) was installed, and wind tunnel systems were checked out. The first run, with hydrogen cooling and SAM inserted in the wind tunnel stream (M = 7.7, P sub TOTAL = 900 psia, T sub TOTAL = 2500 deg R), was accomplished. The condition of the SAM after the run was satisfactory, with no visible signs or data indications of overheating or overloading.
Document ID
19720018062
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
November 24, 1970
Subject Category
Propulsion Systems
Report/Patent Number
NASA-CR-112056
AP-70-6939
ITDR-15
Report Number: NASA-CR-112056
Report Number: AP-70-6939
Report Number: ITDR-15
Accession Number
72N25712
Funding Number(s)
CONTRACT_GRANT: NAS1-6666
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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