Re-entry is studied from standpoints of deceleration, heating, and accuracy of impact for speeds consistent with return from near satellite orbits, and with re-entry from circumlunar orbit under several configurations of lift and constant or variable drag coefficient assumptions; it is shown that deceleration and peak heating rates are not larger than those occurring in ballistic re-entries; total heat input, however, is much larger.


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    Titel :

    On problems of re-entry into earth's atmosphere


    Weitere Titelangaben:

    J Astronautical Sciences


    Beteiligte:
    Robinson, A.C. (Autor:in) / Besonis, A.J. (Autor:in)


    Erscheinungsdatum :

    1960


    Format / Umfang :

    15 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :



    Use of aerodynamic lift during entry into earth's atmosphere

    Lees, L. / Hartwig, F.W. / Cohen, C.B. | Engineering Index Backfile | 1959



    Aerodynamic evidence pertaining to entry of tektites into earth's atmosphere

    Chapman, D.R. / Larson, H.K. / Anderson, L.A. | Engineering Index Backfile | 1962