Study of geometrically similar rockets of different sizes; essential difference between large and small missiles from standpoint of designer; it appears that rocket of 50 tons launching weight might have minimum proportion of deadweight; factors which will set limit to ultimate size of missiles. From paper before High Altitude and Satellite Rocket Symposium.
Design problems of large rockets
Engineer
Engineer ; 204 , n 5295
1957
2 pages
Article (Journal)
English
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