Survey of state of art shows that much of argument about entry vehicles centers on choice of hypersonic maneuverability, or lift-drag (L/D) ratio; parameter is tied closely to both entry performance and to basic physical characteristics of entry vehicles; characteristics of entry vehicles and typical landable configurations; reference made to large-scale free-flight re-entry experiment, Project Fire, designed to obtain critical heating measurements at 37,000 fps; vehicle is 26 in. in diam and weighs 185 lb; tabulation of entry velocities for Mars and Venus Missions.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Entry vehicles


    Weitere Titelangaben:

    Astronautics Aerospace Eng


    Beteiligte:
    Becker, J.V. (Autor:in)


    Erscheinungsdatum :

    1963


    Format / Umfang :

    5 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :



    Earth entry flight test of mars entry vehicles

    BEUF, F. / KATZ, G. / KERN, R. | AIAA | 1965


    Earth entry flight test of mars entry vehicles

    Beuf, F.G. / Katz, G.D. / Kern, R.J. | Engineering Index Backfile | 1966


    Earth entry flight test of Mars entry vehicles.

    BEUF, F. G. / KATZ, G. D. / KERN, R. J. | AIAA | 1966


    Entry vehicles for space programs

    Greenshields, D. H. / Stewart, J. D. | NTRS | 1969