Liquid propulsion systems
Bladder and expulsion devices for spacecraft liquid propulsion systems - pinhole leak test fixture, heat sterilization of ethylene propylene with hydrazine, and metal diaphragms
PROPYLENE↗
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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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Test and evaluation of fuel cell catalysts Quarterly report, Feb. 1 - Apr. 30, 1967
Cathodic catalysts evaluated for hydrazine-air fuel cells employing alkaline electrolytes
Clark, M. B.↗
Test evaluation of fuel cell catalysts Quarterly report, Aug. 16 - Nov. 15, 1967
Corrosion testing of nickel, cobalt, nickel cobalt alloy, borides, and other fuel cell catalyst samples for activity in oxidation of hydrazine
Matsuda, S.↗
Exploratory study of hypergolic ignition spike phenomena, phase 2, part 2, July 1 to September 30, 1966
Chemical analysis, physical properties, and combustion characteristics of hydrazine nitrate
Christos, T.↗
Design, development and demonstration of a warm gas distribution system Quarterly report, period ending 31 Dec. 1967
Development of warm distribution system for hydrazine fueled gas generators for spacecraft attitude control torques
Source record↗
Sterilizable liquid propulsion system Quarterly progress report, 1 Apr. - 30 Jun. 1967
Hydrazine-based bipropellant liquid propulsion system exposed to ethylene oxide and heat sterilization environments
Brady, H. F.↗
Design, development and demonstration of a warm gas distribution system Quarterly report, period ending 31 Mar. 1968
Component tests and system assembly for hydrazine fuel gas distribution system of torque generator for spacecraft attitude control
Boyce, W. D.↗
Post test analysis of generant tank, part no. 9116270-H
Hydrazine and gaseous nitrogen test evaluation of prototype spacecraft tank
Bayce, A. E.↗
Screech suppression techniques for rocket combustors using earth-storable propellants
Injector baffles for flame stability in combustion chambers using nitrogen tetroxide and hydrazine mixture
Bloomer, H. E.↗
A hot gas generator for large scale supersonic combustor testing
Exhaust gas of hydrazine-nitrogen tetroxide rocket for simulating combustor inlet requirements of scramjet engines
Lezberg, E. A.↗
Hypergolic stream impingement phenomena nitrogen tetroxide/hydrazine
Mechanism and design parameter effects in stream mixing and separation of nitrogen tetroxide-hydrazine impingement
Breen, B. P.↗
Preignition phenomena in small A-50/NTO pulsed rocket engines.
Preignition phenomena in small Aerozine-50/ nitrogen tetroxide pulsed rocket engines shown partly due to hydrazine nitrate accumulation
Christos, T.↗
Evidence for the formation of azides in the N sub 2 H sub 4 /N sub 2 O sub 4 reaction.
Azides and hydrazoic acid formation as intermediates involved with pressure spiking when restarting nitrogen tetroxide-hydrazine engines in vacuum
Dauerman, L.↗
Heat release rate for the liquid nitrogen tetroxide/hydrazine reaction by Somogyi and Feiler's method Final report, 19 Jan. - 12 Apr. 1968
Measurement of heat release rate for liquid phase reaction of nitrogen tetroxide and hydrazine
Lawver, B. R.↗
A Basic Study on the Ignition of Hypergolic Liquid Propellants Interim Report
Ignition mechanism of hydrazine-nitrogen dioxide hypergolic propellant system
Breen, B. P.↗
Experimental measurements of expanding storable-propellant products simulated by combustion of gaseous reactants
Gaseous reactant combustion simulation of dimethylhydrazine and hydrazine fuel system for nonequilibrium expansion studies
Friedman, R.↗
A basic study of ignition of hypergolic liquid propellants.
Liquid hydrazine ignition by nitrogen tetroxide gas based on stagnation flow principle, presenting threshold measurements
Breen, B. P.↗
A study of the boundary flow in a rocket combustion chamber. Part 1 - Summary Final report
Boundary flow chemical composition and heat flux data from hydrazine-nitrogen tetroxide rocket engine - Part 1
Grose, R. D.↗