Some considerations in determining the optimum propellant combination for a rocket-powered missile
1949-01-01
4 pages
Article (Journal)
Electronic Resource
English
Optimum staging of solid-propellant rocket vehicles
Engineering Index Backfile | 1961
|Thermal-nucleak powered rocket using non-cryogenic propellant
European Patent Office | 2017
|Some statistical considerations of jet alignment of rocket-powered vehicles
Engineering Index Backfile | 1950
|Optimum climbing technique for rocket-powered aircraft
Engineering Index Backfile | 1955
|