History and development of rocket motors for guided missiles and high-speed aircraft, carried out by BMW (Bayerische Motorenwerke GmbH) in 1939 in specially constructed research and testing plant; types of propellants investigated; BMW's first development in field of non self-igniting propellants was 109-511 motor, design of which had been initiated to overcome deficiencies of Walter 109-507 hydrogen peroxide/permanganate motor powering Hs293 glide bomb; development of Tonka motor.


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    Title :

    Facets of BMW liquid-propellent rocket development 1939-45


    Additional title:

    Spaceflight


    Contributors:
    Kay, A.L. (author)

    Published in:

    Spaceflight ; 9 , n 12


    Publication date :

    1967


    Size :

    4 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :


    Unstable burning in solid propellent rocket motors

    Trubridge, G.F.P. | Engineering Index Backfile | 1965


    Use of solid propellent rocket motors for space application

    Morgan, F.C. / Trubridge, G.F.P. | Engineering Index Backfile | 1967


    Control of rate of thrust build-up in liquid propellent rocket engine

    Bragg, S.L. / Wallace, V.A. | Engineering Index Backfile | 1962


    High Temperature Propellent Reactions

    Osborne, F.E. | Emerald Group Publishing | 1952


    SELF-PROPELLENT CART SYSTEM

    KANNO HIROKI | European Patent Office | 2020

    Free access