Requirements of system which must be capable of functioning under variety of eventualities, including normal and aborted missions; guidelines employed in selection of earth-landing systems for Mercury, Gemini, and Apollo Command Module spacecrafts; development and qualification programs of Mercury spacecraft landing system, including conical, ribbon, drogue parachute, ringsail main and reserve parachutes, impact skirt attenuation system, and deployment methods are described; summary of parachute performance obtained from test programs and results of performance of landing system for 5 manned Mercury flights.


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    Titel :

    Earth-landing systems for manned spacecraft


    Weitere Titelangaben:

    AGARD -- Report


    Beteiligte:
    Kiker, J.W. (Autor:in) / Lee, J.B. (Autor:in) / Hinson, J.K. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1963


    Format / Umfang :

    43 pages


    Medientyp :

    Report


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Design considerations of earth landing systems for manned spacecraft

    Smith, A.M. / Hartung, R.M. / McMullen, J.C. et al. | Engineering Index Backfile | 1963


    Design Considerations of Earth Landing Systems for a Manned Spacecraft

    Cummings, Clifford I. / Lawrence, Harold R. | AIAA | 1963



    LANDING ROCKET - GLIDING PARACHUTE LANDING SYSTEMS FOR MANNED SPACECRAFT

    SUIT, KENNETH / KIKER, JOHN / HINSON, JAMES | AIAA | 1964


    The First Manned Lunar Landing Spacecraft

    Fleisig, R. / International Astronautical Federation | British Library Conference Proceedings | 1994