Loads methods currently being used to design planetary spacecraft to be launched on the shuttle orbiter are summarized. Experiences gained from expendable launch vehicle payloads are used to develop methodologies for the space shuttle orbiter payloads. The objectives for the development of a new methodology for the shuttle payloads are to reduce the cost and schedule for the payload load analysis by decoupling the payload analysis from the launch vehicle to the maximum extent possible. Methods are described for payload member load estimation or obtaining upper bounds for dynamic loads, as well as load prediction or calculating actual transient member load time histories.


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    Title :

    A survey of load methodologies for shuttle orbiter payloads


    Contributors:
    Chen, J. C. (author) / Garba, J. A. (author) / Salama, M. (author) / Trubert, M. (author)

    Conference:

    Conference on Structures, Structural Dynamics and Materials ; 1981 ; Atlanta, GA


    Publication date :

    1981-01-01


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English




    A survey of load methodologies for shuttle orbiter payloads

    Chen, J. C. / Garba, J. A. / Salama, M. et al. | NTRS | 1980



    A Survey of Load Methodologies for Shuttle Orbiter Payloads

    J. C. Chen / J. A. Garba / M. Salama et al. | NTIS | 1980


    Orbiter ECLSS support of Shuttle payloads

    Jaax, J. R. / Morris, D. W. / Prince, R. N. | NTRS | 1974


    Orbiter ECLSS support of shuttle payloads

    Jaax, J. / Morris, D. / Prince, R. | Tema Archive | 1974