An experimental investigation was conducted to determine the feasibility and practicality of the dual rocket motor concept. Cold flow studies were performed with the aid of a ground-test simulator which incorporated a telescoping booster cavity. The effects of booster cavity length, booster cavity shockdown pressure, booster/sustainer nozzle area ratios, and aft nozzle removal on thrust and performance were explored and discussed. (Author)
An Experimental Investigation of the Dual Chamber Rocket
1978
55 pages
Report
No indication
English
An Experimental Investigation of the Dual Chamber Rocket
NTIS | 1979
|Experimental investigation of a lightweight rocket chamber
TIBKAT | 1956
|