Discussion of problem of establishing thrust time relation which will achieve optimum compromise between reduction in gravity and drag losses and thereby result in minimum fuel expenditure.
Optimum thrust programing for high-altitude rockets
Aeronautical Eng Rev
Aeronautical Engineering Review ; 16 , n 6
1957
4 pages
Article (Journal)
English
© Metadata Copyright Elsevier B. V. All rights reserved.
High altitude and satellite rockets
Engineering Index Backfile | 1958
High altitude sounding rockets issue
Engineering Index Backfile | 1957