Method of Calculating Rocket Engine Nozzle Contour for Optimum Thrust
1982
8 pages
Report
Keine Angabe
Englisch
Thrust augmentation nozzle (TAN) concept for rocket engine booster applications
Online Contents | 2006
|Thrust augmentation nozzle (TAN) concept for rocket engine booster applications
British Library Conference Proceedings | 2006
|Nozzle contour optimization for nonuniform rocket flow
AIAA | 1983
|