The patent relates to slurried rocket propellants and a spinning rocket motor wherein the propellants have viscosities which enable them to form central cores when spun in spinning rocket motors. The motor has a diaphragm-like base plate which assists in transferring forward momentum through the propellant. (Author)
Slurried Propellant Rocket Motor
1971
5 pages
Report
Keine Angabe
Englisch
NTIS | 1971
|Liquid-propellant rocket motor
Engineering Index Backfile | 1946
|NTRS | 1973
|Liquid-propellant rocket motor
Engineering Index Backfile | 1946
|