The HEOS-A2 mission will utilize the DSV-3L launch vehicle. A profile of the DSV-3E-7 fairing, showing several points of analysis, is presented. The predicted inner wall temperature histories of the HEOS-A2 fairing are based on a depressed trajectory and the corresponding angle of attack history. (Author)


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    Title :

    Thermal Profiles of the delta Spacecraft Fairings Heos-A2 Thermal Profile, Volume 7


    Contributors:
    L. W. Gale (author)

    Publication date :

    1971


    Size :

    60 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




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