Characteristics of trajectories are examined and factors that determine them, i.e., powered flight phases and geometrical constraints imposed by overall trajectory; geometrical properties that strongly influence ascent trajectory are launch site location, outward radial direction, and launch azimuth; direct ascent and parking orbit types of trajectories are investigated and compared; superiority of parking orbit type is shown having greater payload capability and providing method of launch time delay compensation; injection locations of Mars and Venus trajectories using parking orbits are mapped.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Design of lunar and interplanetary ascent trajectories


    Weitere Titelangaben:

    AIAA J


    Beteiligte:

    Erschienen in:

    AIAA Journal ; 1 , n 7


    Erscheinungsdatum :

    1963


    Format / Umfang :

    9 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :