Role of research rocket and types of vehicle for environmental measurement; design of ballistic rockets; main criteria used in choosing design for Black Knight; development of complete system; first stage has liquid propellant rocket motor using HTP and kerosene which have specific impulse at sea level of 240 sec at 500 lb/sq in.; control and guidance system; second stage; instrumentation; ground facilities; rocket firings.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Ballistic research rockets with particular reference to Black Knight


    Additional title:

    Roy Aeronautical Soc -- J


    Contributors:
    Lyons, D.J. (author)

    Published in:

    Publication date :

    1961


    Size :

    19 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English




    Impact points of ballistic rockets

    Roberson, R.E. | Engineering Index Backfile | 1957



    Method for calculating impact points of ballistic rockets

    Singer, S.F. / Wentworth, R.C. | Engineering Index Backfile | 1957


    EVOLUTIONS IN BALLISTIC DATA RECONSTRUCTION TECHNIQUES FOR HYBRID ROCKETS

    Sicat, Maxime M. / Shimada, Toru / Carmicino, Carmine | TIBKAT | 2021


    Evolutions in Ballistic Data Reconstruction Techniques for Hybrid Rockets

    Sicat, Maxime M. / Shimada, Toru / Carmicino, Carmine | AIAA | 2021