Description A collection of technical papers drawn mainly from the AIAA 3rd Thermophysics Specialist Conference, June 24-26, 1968, subsequently revised for this volume. Topics covered include improved thermal analytical methods and acquisition of necessary data, entry or ablation problems in both earth and planetary spacecraft systems, thermal influence of the on-board orbit injection or descent propulsion system, and the thermal design of a complete system for lunar and Martian vehicles; the thermophysical properties of spacecraft components and of the environment; and the effects of the space environment, real and simulated, upon thermal control materials.


    Access

    Check access

    Check availability in my library

    Order at Subito €


    Export, share and cite



    Title :

    An Approximate Analytic Solution of the Steady-State Thermal Design Problem of Space Radiators


    Contributors:


    Publication date :

    1969-01-01




    Type of media :

    Article/Chapter (Book)


    Type of material :

    Electronic Resource


    Language :

    English





    Steady-State Thermal Design of Space Radiators

    Chapman, A. J. / Lopez, L. | NTRS | 1967



    Thermal Design of the International Space Station Photovoltaic Radiators

    Blaser, Allen N. / Steinfeld, David E. / Flores, Robert R. | SAE Technical Papers | 1998