Analysis of chugging in liquid-bipropellant rocket engines using propellants with different vaporization rates
Model for prediction of low-frequency stability limits for bipropellant rocket engines
PREDICTION THEORY↗
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Search indexed NASA NTRS and DOE OSTI research on propulsion, heat transfer, battery materials and energy systems. Follow report and document links to the original sources.
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Aerothermochemical analysis of non-oscillatory and oscillatory characteristics of liquid bipropellant rocket motors - Wave model, droplet heating, and evaporation program computation Third quarterly report no. 65-1
Aerothermochemical analysis of nonoscillatory and oscillatory characteristics of liquid bipropellant rocket motors - wave model, droplet heating, and evaporation computer program
BIPROPELLANT↗
Steady state aerothermochemistry for liquid bipropellant rocket motors
Model and theoretical equations describing liquid propellant droplet ballistics and combustion gas behavior in bipropellant rocket motors - aerothermochemistry
LIQUID PROPELLANT ROCKET ENGINE↗
Bipropellant pulsed energy turboalternator power system development Final report, Sep. 1, 1965 - Jul. 14, 1966
Development and performance testing of bipropellant pulsed energy turboalternator and gas generator power system
BIPROPELLANT↗
Experimental verification of a double-dead time model describing chugging in liquid bipropellant rocket engines
Experimental verification of double dead time model describing chugging in liquid bipropellant rocket engines
LIQUID PROPELLANT ROCKET ENGINE↗
ANALYTICAL INVESTIGATION OF A BIPROPELLANT ARC JET
Investigation of bipropellant arc jet
SPACECRAFT PROPULSION↗
Experimental verification of a double-dead-time model describing chugging in liquid- bipropellant rocket engines.
Stability boundaries of double-dead-time model describing chugging in liquid bipropellant rocket engine
ANALOG COMPUTER↗
Combustion instability prediction using a nonlinear bipropellant vaporization model
Combustion instability prediction using nonlinear bipropellant vaporization model
Breen, B. P.↗
Experimental investigation of reaction control, storable bipropellant thrustors
Performance of low thrust storable bipropellant thrustors in spacecraft reaction control system
Rollbuhler, R. J.↗
Bipropellant and quadredundant valves, volume 1 Final report
Performance tests on bipropellant and quadredundant propellant valves for rocket engines
Source record↗
Two-stage bipropellant injection system studies Final report
Two stage bipropellant injection with high thrust per injector
Mehegan, P. F.↗
Experimental verification of a double dead time model describing chugging in liquid bipropellant rocket engines
Double dead-time model for combustion stability analysis in liquid bipropellant rocket engines
Szuch, J. R.↗
Semitoroidal-diaphragm cavitating valve designed for bipropellant flow control
Valve controls the flow of bipropellant liquids in rocket engines. Throttling and cavitation of the liquids are controlled by axial deflections of a semitoroidal metal diaphram. The valve is highly resistant to corrosion and leakage, and should be useful in food processing and chemical industries.
Young, A. L.↗
Two-step rocket engine bipropellant valve concept
Initiating combustion of altitude control rocket engines in a precombustion chamber of ductile material reduces high pressure surges generated by hypergolic propellants. Two-step bipropellant valve concepts control initial propellant flow into precombustion chamber and subsequent full flow into main chamber.
Capps, J. E.↗
Performance investigation of bipropellant fractional-pound thrusters
Performance of bipropellant fractional-pound rocket thrustor
Rollbuhler, R. J.↗
Two-step rocket engine bipropellant valve Patent
Solenoid two-step valve for bipropellant flow rate control to rocket engine
Capps, J. E.↗
Injector for bipropellant rocket engines Patent
Injector manifold assembly for bipropellant rocket engines providing for fuel propellant to serve as coolant
Heidmann, M. F.↗