Total weight requirements for three types of manned, round trip, soft landing lunar missions are investigated, all starting out from space station circling Earth at altitude of 350 mi; first and second missions follow direct hit flight trajectories and employ chemical and nuclear power plants; third uses nuclear power to reach circular orbit around moon, whereas for landing and ascent portions final payload is propelled by chemical rockets.


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    Titel :

    Some weight considerations for manned lunar missions


    Weitere Titelangaben:

    ARS -- J


    Beteiligte:

    Erschienen in:

    Erscheinungsdatum :

    1960


    Format / Umfang :

    3 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Some general considerations of manned lunar return missions

    Eggers, Jr., A.J. / Wong, T.J. / Hornby, H. et al. | Engineering Index Backfile | 1963


    Some General Considerations of Manned Lunar Return Missions

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


    SOME GENERAL CONSIDERATIONS OF MANNED LUNAR RETURN MISSIONS

    Eggers, A. J., Jr. / Hornby, H. / Wong, T. J. et al. | NTRS | 1963


    Abort considerations for manned lunar missions

    Kelly, T.J. / Adornato, R.J. / Speiser, R.H. | Engineering Index Backfile | 1963


    Abort Considerations for Manned Lunar Missions

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