Details of Thor intermediate-range ballistic missile which is vehicle portion of Weapon System 315A; notes on design and development program by Douglas Aircraft Co, Santa Monica, Calif; aspects of Thor operation; propulsion is provided by Rocketdyne MB-2 rocket engine of 150,000 lb thrust at sea level, operating on liquid oxygen and RP-1 fuel; cutaway drawing. (see also Aeroplane and Astronautics v 96 n 2490 May 22 1959 p 597-600)


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    Title :

    Thors for R.A.F


    Additional title:

    Flight


    Published in:

    Flight ; 75 , n 2626


    Publication date :

    1959


    Size :

    3 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :


    Thors for R.A.F

    Engineering Index Backfile | 1959


    R.A.F. casualties

    Engineering Index Backfile | 1929


    R.A.F. instruction

    Engineering Index Backfile | 1940


    R.A.F. over Burma

    Engineering Index Backfile | 1944


    Power behind R.A.F.

    Engineering Index Backfile | 1933