Description This volume is devoted to the science and technology associated with spacecraft thermal control and as such it is dominated by the topic of radiative transfer. The thermal performance of a system in space depends upon the radiative interaction between external surfaces and the external environment (space, exhaust plumes, the sun) and upon the management of energy exchange between components within the spacecraft environment. The volume presents a view of timely advances in spacecraft radiative transfer and temperature control, which was drawn from the thermophysics sessions at the AIAA 19th Aerospace Sciences Meeting in St. Louis, MO in January 1981, and the AIAA 16th Thermophysics Conference in Palo Alto, CA in June 1981. These papers have been revised, updated, and organized into six coherent chapters that discuss heat transfer and properties, plume radiance, contamination and degradation, temperature control components, complex systems, and future concepts.


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    Titel :

    Calculation of Visible Radiation from Missile Plumes


    Beteiligte:
    Horton, T. E. (Autor:in)


    Erscheinungsdatum :

    01.01.1982




    Medientyp :

    Aufsatz/Kapitel (Buch)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch




    Preventing Aircraft Damage Due to Missile Exhaust Plumes

    Dennis, C. / Royal Aeronautical Society | British Library Conference Proceedings | 2007



    Simulation of Missile Plumes for Aircraft Store Compatibility Assessments

    Gleissl, R. / Deslandes, R. M. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2005


    Scattered visible and ultraviolet solar radiation from condensed attitude control jet plumes

    KOLB, C. E. / LYONS, R. B. / ELGIN, J. B. et al. | AIAA | 1983