NASA NTRS · 19720018062
Hypersonic research engine project. Phase 2: Structures and cooling development
Abstract
The 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.
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Jilly, L. F.. 1970-11-24. Hypersonic research engine project. Phase 2: Structures and cooling development. https://ntrs.nasa.gov/citations/19720018062
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