Sept. Design objectives of small solid-propellant satellite launcher comprised high reliability, ease of development, high performance, and low cost per pound of satellite weight; development of solid propellant, four-stage rocket, with inertial and celestial guidance; basic engine has case-bonded grain, burning takes place on surface of six-pointed-star port; description of engine structure, guidance system, and propellant characteristics. Nov. Control features, range safety, reliability and orbits are described. (n 5 Sept 1965 p 146-154)


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Minimum-cost satellite launcher


    Weitere Titelangaben:

    Spaceflight


    Beteiligte:
    Godwin, F. (Autor:in)

    Erschienen in:

    Spaceflight ; 7 , n 6


    Erscheinungsdatum :

    1965


    Format / Umfang :

    5 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Intrepid-A Low Cost Small Satellite Launcher

    French, J. R. / Ingersoll, T. / IEEE; Aerospace and Electronics Systems Society | British Library Conference Proceedings | 1998


    Intrepid-a low cost small satellite launcher

    French, J.R. / Ingersoll, T. | IEEE | 1998


    TECHNICAL CONSTRAINTS FOR A LOW-COST FEMTO-SATELLITE LAUNCHER

    Jove-Casulleras, R. / Tristancho, J. / Vera-Flores, C. et al. | British Library Conference Proceedings | 2011


    Technical Constraints for a Low-Cost Femto-Satellite Launcher

    Jove-Casulleras, Roger / Tristancho, Joshua / Vera-Flores, Carlos | AIAA | 2011


    DSI Small Satellite Launcher

    S. Nichols / D. Gibbons / J. Wise et al. | NTIS | 1992