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.


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    Titel :

    Hypersonic, Diffusion-Controlled Oxidation of Tungsten


    Beteiligte:


    Erscheinungsdatum :

    1969-01-01


    Format / Umfang :

    23 pages




    Medientyp :

    Aufsatz/Kapitel (Buch)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch




    Analysis of nosetip recession of the tungsten projectiles in hypersonic flight

    CHIANG, TING / HOFFMANN, KLAUS / SIDDIQUI, M. | AIAA | 1993


    Molecular-Scale Carbon Oxidation at Hypersonic Speeds

    Schmitt, Simon / Graña-Otero, José / Mahmoudi, Siamak | AIAA | 2019


    Evaluation of multicomponent diffusion effects in hypersonic flows

    Rasmussen, Maurice / Yoon, Bokhyun | AIAA | 1997