For preliminary studies of space vehicle configurations during entry into planetary atmospheres, it is convenient to obtain rapid estimates of heating data from desk calibrations; method is presented as first phase of continuing effort to develop preliminary studies of lifting re-entry configurations independent of rigid numerical trajectory analysis; method provides only approximate solution to 2 simultaneous nonlinear differential equations that characterize trajectory problem.


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    Titel :

    Implications of re-entry trajectory control on vehicle design criteria at superorbital speeds


    Weitere Titelangaben:

    SAE -- Paper


    Beteiligte:
    Bell, R.W. (Autor:in) / Hung, F.C.S. (Autor:in)

    Kongress:

    SAE Meeting ; 1962 Re-entry



    Erscheinungsdatum :

    1962


    Format / Umfang :

    7 pages


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Implications of Re-Entry Trajectory Control on Vehicle Design Criteria at Superorbital Speeds

    Hung, Francis C. S. / Bell, Richard W. | SAE Technical Papers | 1962


    Variable-lift re-entry at superorbital and orbital speeds

    Wang, H.E. / Chu, S.T. | Engineering Index Backfile | 1963


    Non-lifting entry-vehicle design for superorbital velocities

    Ambrosio, A. / Baer, D.H. / Myer, H.G. | Engineering Index Backfile | 1963