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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    Title :

    Hypersonic research engine project. Phase 2: Aerothermodynamic Integration Model (AIM) test report


    Contributors:
    Andersen, W. L. (author) / Kado, L. (author)

    Publication date :

    1975-05-19


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English