Problems encountered and solved successfully in design of Viking RTV-N-12a with reaction motors XLR 10-RM-2 liquid oxygen and alcohol rocket engine producing 21,000 lb thrust at sea level for research at altitudes between 100 and 200 mi.
Aerodynamic design of high-altitude rocket
Aeronautical Eng Rev
Aeronautical Engineering Review ; 14 , n 4
1955
5 pages
Article (Journal)
English
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