Optimum weight distribution for rockets having different specific impulses and structural factors in each stage is derived; minimization of gross weight for given required burnout velocity and payload is criterion of optimization used; method suggested for including in first approximation, effects of gravity, drag and turn.
On optimization of multistage rockets
Jet Propulsion
Jet Propulsion ; 28 , n 7
1958
3 pages
Article (Journal)
English
© Metadata Copyright Elsevier B. V. All rights reserved.
Cost Optimization of Multistage Rockets
NTIS | 1967
|Cost optimization of multistage rockets
NTRS | 1967
|Optimization of multistage rockets including drag
AIAA | 1970
|Optimization analysis of multistage solid rockets
AIAA | 1982
|Cost and weight optimization for multistage rockets
Engineering Index Backfile | 1965
|