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:
    Bouslog, Stan (Autor:in) / Rochelle, Bill (Autor:in) / Williams, Stan (Autor:in) / Caram, Joe (Autor:in) / Curry, Don (Autor:in) / Derry, Steve (Autor:in) / Ondler, Matt (Autor:in)


    Erscheinungsdatum :

    1992-01-01


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch




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