Dr. Chapman's lecture examines the physics behind spacecraft entry into planetary atmospheres. He explains how scientists determine if a planet has an atmosphere and how scientists can compute deceleration when the atmospheric conditions are unknown. Symbols and equations used for calculations for aerodynamic heating and deceleration are provided. He also explains heat transfer in bodies approaching an atmosphere, deceleration, and the use of ablation in protecting spacecraft from high temperatures during atmospheric entry.


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    Titel :

    Aerodynamic Heating and Deceleration During Entry into Planetary Atmospheres


    Beteiligte:

    Erscheinungsdatum :

    10.04.1962


    Medientyp :

    Audiovisuelles Material


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


    Entry into planetary atmospheres

    Roberts, L. | Engineering Index Backfile | 1964


    Radiating flows during entry into planetary atmospheres.

    Boughner, R. E. / Burns, R. K. / Goulard, R. et al. | NTRS | 1968




    An analytic solution for entry into planetary atmospheres

    CITRON, S. J. / MEIR, T. C. | AIAA | 1965