The feasibility of using the space shuttle to launch planetary and DoD entry flight experiments was examined. The results of the program are presented in two parts: (1) simulating outer planet environments during an earth entry test, the prediction of Jovian and earth radiative heating dominated environments, mission strategy, booster performance and entry vehicle design, and (2) the DoD entry test needs for the 1980's, the use of the space shuttle to meet these DoD test needs, modifications of test procedures as pertaining to the space shuttle, modifications to the space shuttle to accommodate DoD test missions and the unique capabilities of the space shuttle. The major findings of this program are summarized.


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    Title :

    Planetary/DOD entry technology flight experiments. Volume 1: Executive summary


    Contributors:

    Publication date :

    1976-02-29


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English


    Keywords :


    Planetary/DoD Entry Technology Flight Experiments. Volume 1: Executive Summary

    H. E. Christensen / R. J. Krieger / W. R. Mcneilly et al. | NTIS | 1976


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    H. E. Christensen / R. J. Krieger / W. R. Mcneilly et al. | NTIS | 1976


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    Christensen, H. E. / Krieger, R. J. / Mcneilly, W. R. et al. | NTRS | 1976


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    Christensen, H. E. / Frieger, R. J. / Mcneilly, W. R. et al. | NTRS | 1976


    Planetary/DoD Entry Technology Flight Experiments. Volume 4: DoD Entry Flight Experiments

    H. E. Christensen / R. J. Krieger / W. R. Mcneilly et al. | NTIS | 1976