Flight calculations presented showing that, with existing fuels and jet exhaust, 4-stage rocket with takeoff weight of 600 tons, can reach upper orbiting velocity and altitude; design of Von Braun's 3-stage 7000-ton rocket. (See also - discussion p L42-5)
Problems of interplanetary travel
Enige beschouwingen over het ruimtevaart-probleem
Ingenieur ; 64 , n 46
1952
Article (Journal)
Dutch
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