Direct and indirect abort trajectory requirements of lunar orbit and descent phase of manned lunar mission; indirect aborts, treated through intermediate lunar parking orbit, are shown to be possible from any point on trajectory down to final touchdown, but regions from which direct aborts can commence are restricted; velocity increment and time-to-return for direct and indirect abort sequences are established with emphasis on initial trajectory.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Abort considerations for manned lunar missions


    Weitere Titelangaben:

    Progress Astronautics Aeronautics


    Beteiligte:
    Kelly, T.J. (Autor:in) / Adornato, R.J. (Autor:in) / Speiser, R.H. (Autor:in)


    Erscheinungsdatum :

    1963


    Format / Umfang :

    32 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Abort Considerations for Manned Lunar Missions

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


    Some weight considerations for manned lunar missions

    Schechter, H.B. | Engineering Index Backfile | 1960


    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