The unusual features of the Ultrahigh Altitude Rocket Cell J-2A at Arnold Engineering Development Center are described with emphasis on the cryogenic systems for cooling the diffuser and chamber liner to liquid-nitrogen temperature and the helium-refrigerated cryopumping surfaces to 20 K. It is concluded that space simulation testing of large rocket engines under actual firing conditions is possible.


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    Titel :

    Cryogenics as Applied to the Design and Fabrication of a Space Simulation Test Cell at the Arnold Engineering Development Center*


    Weitere Titelangaben:

    Sae Technical Papers


    Beteiligte:
    Ansley, S. P. (Autor:in)

    Kongress:

    Pre-1964 SAE Technical Papers ; 1906



    Erscheinungsdatum :

    1962-01-01




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch




    Arnold engineering development center

    Wild, J.M. | Engineering Index Backfile | 1957


    The Arnold Engineering Development Center

    CARROLL, F. O. | SAE Technical Papers | 1950


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    Lizon-Tati, J. | Elsevier | 1983


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    Smith, R. W. / SPIE | British Library Conference Proceedings | 1995


    Aeropropulsion Test Capability at the Arnold Engineering Development Center (AEDC)

    Danhof, R. / Turrentine, A. / International Society for Air Breathing Engines; United States Committee | British Library Conference Proceedings | 1997