The preflight mission design and in-flight execution are presented to illustrate the actual utilization of the adaptive nature of this mission. Spacecraft systems (propulsion, attitude, accelerometer) and software (maneuver program) features which contribute to the adaptive trajectory flexibility are discussed. Descriptions of procedures used to handle low perigee maneuver operations (to 130 km), for achieving ground track control and orbit phasing, for making a transition from elliptical to circular orbits, and for circular orbit restoration and maintenance are presented in detail. The 85 maneuvers made during the first 17 months of the mission are summarized.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Atmosphere explorer /AE-C/ adaptive mission design and trajectory performance


    Beteiligte:
    Barbieri, R. W. (Autor:in) / Cooley, J. L. (Autor:in) / Nickerson, K. G. (Autor:in)

    Kongress:

    Astrodynamics Specialist Conference ; 1975 ; Nassau, Bahamas


    Erscheinungsdatum :

    01.07.1975


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


    The Atmosphere Explorer Mission

    Dalgarno, A. / Hanson, W.B. / Spencer, N.W. et al. | Tema Archiv | 1973


    The Lunar Atmosphere and Dust Environment Explorer (LADEE) Mission

    Spremo, Stevan / Turner, Mark / Caffrey, Robert T. et al. | NTRS | 2010



    Mission Design for the Innovative Interstellar Explorer Vision Mission

    Fiehler, Douglas I. / McNutt, Ralph L. | NTRS | 2005