Structural and aerodynamic concepts for centrifugally deployed, variable-geometry atmospheric entry aids are discussed which include means for controlling apex angle of centrifugally stabilized conical flight bodies, concept of isothermal flight, i.e., atmospheric entry at constant surface temperature, and analytical design of optimum rotor-blade structures; materials for flexible rotor construction are classified according to temperature-strength parameter that is characteristic for intended application; application of entry rotor concept to Mars and Earth landing capsule is presented in form of conceptual design configuration. (See also J Spacecraft and Rockets v 2 n 4 July-Aug 1965 p 523-30)


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    Title :

    Low-density, autorotating wings for manned re-entry


    Additional title:

    AIAA -- Tech Papers


    Contributors:

    Conference:

    Meeting of the AIAA -- Engineering Problems of Manned Interplanetary Exploration ; 1963 Re-entry



    Publication date :

    1963


    Size :

    29 pages


    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English


    Keywords :