Study of 3-stage composite, earth satellite launching system; first stage provides power for takeoff, initial climb and acceleration to second stage ramjet starting velocity; 2 trajectories of second stage (recoverable, ramjet powered lifting vehicle) are computed on IBM 650 computer; third stage is rocket which takes its payload to orbital conditions; report is devoted mainly to performance of second stage; ramjet performance analysis and performance scaling factor.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Air-breathing satellite booster


    Weitere Titelangaben:

    Can Aeronautical J


    Beteiligte:
    Wu, J.H.T. (Autor:in) / Molder, S. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1961


    Format / Umfang :

    7 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Air-breathing booster

    Engineering Index Backfile | 1962


    Design aspects of air breathing booster

    Bond, W.H. / Mawhinney, R.F. | Engineering Index Backfile | 1960


    Design aspects of air breathing booster

    Bond, W.H. / Mawhinney, R.F. | Engineering Index Backfile | 1960


    DESIGN ASPECTS OF AN AIR BREATHING BOOSTER

    MAWHINNEY, R. F. / BOND, W. H. | SAE Technical Papers | 1960


    Inserted Type Solid Rocket Booster Separation from an Air Breathing Engine Vehicle

    Choi, Jong ho / Yoon, Hyeon-Gull / Lim, Jin-shik | AIAA | 2009