Unpowered, unconstrained object is considered to be ejected impulsively with low speed from satellite in circular orbit; ejection velocity vector has arbitrary direction within satellite's orbital plane; equations are developed describing object's motion relative to frame of reference centered on satellite for case that atmospheric drag acts on object; trajectories (obtained on analog computer) are illustrated by plots applying to 2 objects having different values of ballistic drag parameter and to low speed ejection and zero speed release.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Relative trajectories of objects ejected from near satellite


    Weitere Titelangaben:

    AIAA J


    Beteiligte:
    Knoliman, G.C. (Autor:in) / Pyron, B.O. (Autor:in)

    Erschienen in:

    AIAA Journal ; 1 , n 2


    Erscheinungsdatum :

    1963


    Format / Umfang :

    6 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    RELATIVE TRAJECTORIES OF OBJECTS EJECTED FROM A NEAR SATELLITE

    KNOLLMAN, G. C. / PYRON, B. O. | AIAA | 1963


    Trajectories of objects ejected from aircraft

    Korsak, K. | Engineering Index Backfile | 1960


    SYSTEM TO DETECT OBJECTS EJECTED FROM VEHICLE

    WILDEMANN SOEREN | Europäisches Patentamt | 2021

    Freier Zugriff

    System to detect objects ejected from a vehicle

    WILDEMANN SÖREN | Europäisches Patentamt | 2021

    Freier Zugriff

    SYSTEM TO DETECT OBJECTS EJECTED FROM A VEHICLE

    WILDEMANN SÖREN | Europäisches Patentamt | 2021

    Freier Zugriff