Lunar injection conditions that are required to establish Earth-return trajectories satisfying specified reentry conditions are presented; it is assumed that return trajectory is initiated either from circular lunar orbit having arbitrary inclination and nodal position with respect to Earth-Moon plane or from arbitrary position on lunar surface; in latter case, it is further assumed that lunar parking orbit is established prior to injection.


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    Titel :

    Trajectory considerations for return to earth phase of lunar missions


    Weitere Titelangaben:

    Progress Astronautics Aeronautics


    Beteiligte:
    Gapcynski, J.P. (Autor:in) / Tolson, R.H. (Autor:in)


    Erscheinungsdatum :

    1963


    Format / Umfang :

    16 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Trajectory Considerations for the Return to Earth Phase of Lunar Missions

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




    Trajectory and Guidance Considerations for Lunar Return Missions

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


    Trajectory and guidance considerations for lunar return missions

    Magness, T.A. / Pace, Jr., W.H. / Penzo, P.A. et al. | Engineering Index Backfile | 1963