NASA NTRS · 19720018065
Hypersonic research engine project. Phase 2: Aerothermodynamic integration model development
Abstract
The 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.
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Jilly, L. F.. 1971-03-30. Hypersonic research engine project. Phase 2: Aerothermodynamic integration model development. https://ntrs.nasa.gov/citations/19720018065
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