Experiments have been conducted with a jacketed rocket combustion chamber that was fabricated by hydraulic-forming from sheet metal. Rocket combustion chambers made by this method have been used successfully. Runs with these combustion chambers have been made at over-all heat-transfer rates 1.7 Btu per square inch per second with water cooling and also ammonia as a regenerative coolant.
Experimental investigation of a lightweight rocket chamber
1953-10-01
Miscellaneous
No indication
English
An Experimental Investigation of the Dual Chamber Rocket
NTIS | 1979
|An Experimental Investigation of the Dual Chamber Rocket
NTIS | 1978
|