Dynamic problems of system stability and control considered are illustrated by reference chiefly to hydrogen-oxygen rocket; pressure-fed and pump-fed rocket systems; elements of rocket that contribute significantly to system dynamics are turbopump cooling jacket, flexible injector head and combustion dynamics; effects of component dynamics on system stability, design, operation, and control are illustrated.
Dynamics and control of chemical rockets
NASA -- Proc
NASA -- University Conference on Science and Technology of Space Exploration ; 1962 Control
1962
4 pages
Conference paper
English
© Metadata Copyright Elsevier B. V. All rights reserved.
AIAA | 1997
|Separation Dynamics of Ullage Rockets
Online Contents | 1994
|Separation dynamics of ullage rockets
AIAA | 1994
|Dynamics of rockets and satellites
TIBKAT | 1965
|Engineering Index Backfile | 1966
|