A computer program for simulating optimized space shuttle trajectories is presented. The program considers the ascent, return, and synergetic maneuvers of lifting boosters and spacecraft. Other constraints on optimum trajectory such as maximum heating, acceleration, angle of attack, and excluded or included overflight or impact regions are examined. Mathematical models are included to support the theoretical aspects of the discussion.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Optimized space shuttle trajectory simulation


    Beteiligte:
    Tramonti, L. (Autor:in) / Brusch, R. G. (Autor:in)


    Erscheinungsdatum :

    1972-02-01


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


    Shuttle-optimized space motor technology

    KIRSCHNER, T. / LUSHIS, D. / PHILLIPS, O. | AIAA | 1980





    Space Shuttle Day-of-Launch Trajectory Design Operations

    Harrington, Brian / Picka, Bret / Cordova, Henry | AIAA | 2011