A thermal protection study was conducted on the first lunar outpost (FLO) crew module. The study objectives are as follows: (1) assess effects of vehicle size on aerothermodynamic environment and thermal protection system (TPS) weight; (2) assess effects of lunar-return strategies on aerothermodynamic environment and TPS weight; and (3) assess weight penalty for common TPS design for all lunar-return strategies. All material is covered in viewgraph format.


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    Titel :

    First Lunar Outpost Crew Module Thermal Protection Design Sensitivity


    Beteiligte:
    S. Bouslog (Autor:in) / B. Rochelle (Autor:in) / S. Williams (Autor:in) / J. Caram (Autor:in) / D. Curry (Autor:in)

    Erscheinungsdatum :

    1992


    Format / Umfang :

    15 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




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