NASA NTRS · 19750018941
Hypersonic research engine project. Phase 2: Aerothermodynamic Integration Model (AIM) test report
Abstract
The Hypersonic Research Engine-Aerothermodynamic Integration Model (HRE-AIM) was designed, fabricated, and tested in the Hypersonic Tunnel Facility. The HRE-AIM is described along with its installation in the wind tunnel facility. Test conditions to which the HRE-AIM was subjected and observations made during the tests are discussed. The overall engine performance, component interaction, and ignition limits for the design are evaluated.
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Andersen, W. L., Kado, L.. 1975-05-19. Hypersonic research engine project. Phase 2: Aerothermodynamic Integration Model (AIM) test report. https://ntrs.nasa.gov/citations/19750018941
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