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Hypersonic research engine project. Phase 2: Aerothermodynamic integration model developmentThe fabrication of the various components of the HRE AIM was completed. The purge system necessary for the cavity bounded by the outer shell assembly and the outer cowl body was studied. Preparations were begun for establishing a format for test data acquisition and reduction.
Document ID
19720018065
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
March 30, 1971
Subject Category
Propulsion Systems
Report/Patent Number
NASA-CR-112060
ITDR-12
AP-71-7279
Report Number: NASA-CR-112060
Report Number: ITDR-12
Report Number: AP-71-7279
Accession Number
72N25715
Funding Number(s)
CONTRACT_GRANT: NAS1-6666
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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