RESULTS OF THEORETICAL ROCKET-MOTOR-PERFORMANCE CALCULATIONS FOR LIQUID-PROPELLANT SYSTEMS
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Elverum, G. W., Jr.↗
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Results for “LIQUID PROPELLANT”
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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Velocity of sound in liquid propellants
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Odgers, I. L.↗
Transient pressure measurements in liquid propellant rocket thrust chambers.
Transient pressure measurements in rocket thrust chambers used in propulsion systems research
TRANSIENT PRESSURE↗
Factors which influence the stability of liquid propellants as rocket motor regenerative coolants
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Bartz, D. R.↗
An analysis of oscillatory flow in liquid- propellant rocket feed systems and the application of the analysis to combustion stability
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Wick, R. S.↗
Compatibility of titanium with liquid propellants
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Chafey, J. E.↗
Computer program provides steady state analysis for liquid propellant propulsion systems
Computer program uses Bernoullis formula and Newton-Raphson method to provide steady state fluid flow analysis of line pressure drop in a system with six outlets for each of two main storage tanks. Program flexibility arises in the ease with which changes in the fluid line geometry can be made.
Clark, R. L.↗
Liquid propellant thermal conditioning system Interim report
Venting system for use with cryogenic propellants to control tank pressure during zero-gravity coast
PRESSURE REGULATOR↗
Liquid propellant tests in a vacuum chamber Final report, 7 Jun. 1966 - 7 Jun. 1967
Reactivity and expansion characteristics of Aerozine-50 and nitrogen tetroxide from vacuum chamber tests
AEROZINE↗
Exploring in aerospace rocketry. 7 - Liquid propellant rocket systems
Operating characteristics and design aspects of injector, combustion chamber, and exhaust nozzle for bipropellant rockets
Conrad, E. W.↗
Producing holograms of reacting sprays in liquid propellant rocket engines, phase 2 Interim report, 3 Apr. - 2 May 1968
Pulsed ruby laser holograms of hypergolic rocket propellants combustion processes
Matthews, B. J.↗
Radiation effects on liquid propellants quarterly report
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Kircher, J. F.↗
A Basic Study on the Ignition of Hypergolic Liquid Propellants Interim Report
Ignition mechanism of hydrazine-nitrogen dioxide hypergolic propellant system
Breen, B. P.↗
Statistical Analysis of Project Pyro Liquid Propellant Explosion Data
Statistical regression analysis of Project Pyro cryogenic propellant explosion test data
Andersen, G. R.↗
A basic study of the ignition of hypergolic liquid propellants Final report
Theoretical analysis of ignition mechanisms and quantitative analysis of vapor phase reaction products of dimethylhydrazines with nitrogen dioxide
Breen, B. P.↗
A study of high frequency nonlinear combustion instability in baffled annular liquid propellant rocket motors
Computer program contains mathematical model which provides relationship between engine gas dynamics and combustion processes. Mathematically simulated explosions initiate gas disturbances. Design methods for damping disturbances can be studied to prevent future engine shutdown or destruction.
Abreu, A.↗
Radiation effects on liquid propellants, part 2 Final report
Effects of radiation on stability and compatibility of hydrazine and hydrazine-24 percent hydrazine nitrate in stainless steel and titanium alloy containers with O ring seals
Kircher, J. F.↗
A plan for a material compatibility program for oxygen difluoride (OF sub 2) and diborane (B sub 2 H sub 2) liquid propellants
Evaluation of metallic and nonmetallic construction material performance and reliability after long storage in OF2 and B2H6
Denson, J. R.↗