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- W131418043 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." @default.
- W131418043 created "2016-06-24" @default.
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- W131418043 date "1975-05-19" @default.
- W131418043 modified "2023-09-25" @default.
- W131418043 title "Hypersonic research engine project. Phase 2: Aerothermodynamic Integration Model (AIM) test report" @default.
- W131418043 hasPublicationYear "1975" @default.
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