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.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Air-breathing satellite booster


    Additional title:

    Can Aeronautical J


    Contributors:
    Wu, J.H.T. (author) / Molder, S. (author)

    Published in:

    Publication date :

    1961


    Size :

    7 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :


    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