Problems were investigated on fixed base simulator for blunt face, high drag capsule and low drag lifting cone, each having trim lift drag ratio of 0.5; re-entries were made within constraints of acceleration and skipping, in which pilot was given simulated navigation tasks of altitude and heading angle commands; results for various damper failure conditions.


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    Title :

    Dynamic stability and control problems of piloted reentry from lunar missions


    Additional title:

    NASA -- Tech Notes


    Contributors:
    Moul, M.T. (author) / Schy, A.A. (author) / Williams, J.L. (author)


    Publication date :

    1961


    Size :

    20 pages


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :


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