In missile preliminary design it is necessary to quickly and economically estimate the aerodynamics of a wide variety of missile configuration designs. Since the ultimate shape and aerodynamic performance are so dependent upon the subsystems utilized, such as payload size, propulsion system selection and launch mechanism, the designer must be capable of predicting a wide variety of configurations accurately. The fundamental purpose of Missile Datcom is to provide an aerodynamic design tool which has the predictive accuracy suitable for preliminary design, and the capability for the user to easily substitute methods to fit specific applications.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Missile Datcom User's Manual. Revision, 6/93


    Beteiligte:
    K. A. Burns (Autor:in) / K. J. Deters (Autor:in) / S. L. Stoy (Autor:in) / S. R. Vukelich (Autor:in) / W. B. Blake (Autor:in)

    Erscheinungsdatum :

    1993


    Format / Umfang :

    248 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Missile Datcom User's Manual - 2008 Revision

    L. Auman / J. Doyle / C. Rosema et al. | NTIS | 2008



    Missile Datcom. User's Manual - Rev 4/91

    K. D. Bruns / M. E. Moore / S. L. Stoy et al. | NTIS | 1991


    Recent Improvements to Missile DATCOM

    Underwood, M. / Rosema, C. / Wilks, B. et al. | British Library Conference Proceedings | 2007


    Missile DATCOM. Volume 1

    S. R. Vukelich / S. L. Stoy / K. A. Burns et al. | NTIS | 1988