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US2749706A
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Mechanism for cooling a combustion chamber in propulsion apparatus and for feeding combustion liquids thereto
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US2760335A
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Apparatus for continuously feeding a liquid fuel and a liquid oxidizer to a combustion chamber of propulsion type and having an open discharge nozzle
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US2770251A
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Quick-acting reducing valve
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US2749884A
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Pressure-operated feeding apparatus for combustion liquids in an internal combustionchamber
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US2770255A
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Dual-range safety valve
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US2695496A
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Structure for feeding, intermingling, vaporizing, and igniting combustion liquids ina combustion chamber for rocket-type propulsion apparatus
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US2717182A
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Shaft-positioning mechanism for turbine-driven pumps
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US2718899A
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Quick-acting shut-off valve
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US2633700A
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Combustion chamber for propulsion apparatus and having multiple discharge nozzles
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US2674848A
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Combustion chamber with multiple target recesses for use in rocket apparatus
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US2627876A
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Venturi control for liquid flow
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US2667740A
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Means for supplying and cooling rocket type combustion chambers
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US2624360A
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Proportionate flow control by balanced magnetic force
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US2651171A
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Propulsion apparatus actuated by successive charges of detonating materials
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US2633699A
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Propulsion apparatus actuated by successive charges of detonating materials
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US2551115A
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Hollow partition between premixing and combustion chambers for rockets
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US2563029A
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Jacketed reaction nozzle with hollow spiral vanes for rocket motors
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US2612752A
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Feeding apparatus, including injectors adapted to supply combustion liquids under pressure to a combustion chamber
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US2558484A
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Cooling jacket and heat-resistant cap for combustion chambers
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US2528134A
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Circuit closing device for fuel feed apparatus and having quick-acting thermal control
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