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
© Metadata Copyright Elsevier B. V. All rights reserved.
Special rockets and pyrotechnics problems
Engineering Index Backfile | 1961
|Ascent Problems of Sounding Rockets
NTIS | 1961
|Special Rockets and Pyrotechnics Problems
NTIS | 1961
|Ascent Problems of Sounding Rockets
NTRS | 1961
|Special Rockets and Pyrotechnics Problems
NTRS | 1961
|