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 Flight v 75 n 2626 May 22 1959 p 713-15)
Thors for R.A.F
Aeroplane Astronautics
Aeroplane and Astronautics ; 96 , n 2490
1959
4 pages
Article (Journal)
English
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Engineering Index Backfile | 1959
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