Regenerative-cooling Studies in a 5000-pound-thrust Liquid-oxygen - JP-4 Rocket Engine Operated at 600-pounds-per-square-inch Combustion-chamber Pressure
01.01.1956
Sonstige
Keine Angabe
Englisch
Pounds or pounds per square inch -- I
Engineering Index Backfile | 1936
|Transpiration Cooling of Rocket Thrust Chamber with Liquid Oxygen
British Library Conference Proceedings | 1998
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