Flight and experimental expulsion bladders for Mariner 69 Final report
Synthetic rubber polymer compounds and fabrication of hydrazine expulsion bladders for Mariner 69
Repar, J.↗
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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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Thermometric determination of oxidant-fuel distribution within a rocket combustor
Tungsten-rhenium alloy thermocouples to determine distribution of hydrazine-nitrogen tetroxide products within combustion chamber
Burrows, M. C.↗
Planetary exploration SRT - Advanced technical development
Berylliumized propellant and hydrazine vernier engine for Jupiter Orbiter propulsion system
Source record↗
Ignition means for monopropellant Patent
Catalyst bed ignition system for hydrazine propellants
Evans, D. D.↗
Optimum mixing of hypergolic propellants in an unlike doublet injector element
Optimum penetration and separation mixing of unlike doublet injector element with hypergolic hydrazine and nitrogen tetroxide propellants
Houseman, J.↗
Ratio of disproportionation to combination of N2H3 radicals
Disproportionation to combination ratio of hydrazyl radicals generated in absence of hydrazine direct decomposition
Stief, L. J.↗
Reactive stream separation photography
Reactive stream separation high speed color photography for impinging streams of nitrogen tetroxide and hydrazine
Campbell, D. T.↗
Task 6 storable propellant module environmental control technology Summary report
Thermal control concepts for space storable fluorine hydrazine propulsion module
De Land, R. R.↗
Throttleable thrustor system Final report
Developing throttleable monopropellant hydrazine thrustor system for planetary landing vehicles
Kenny, R. J.↗
Solder flux which leaves corrosion-resistant coating Patent
Hydrazine monoperfluoro alkanoate solder flux leaving corrosion resistant coating, for metals such as copper
Bauman, A. J.↗
Soldering with solder flux which leaves corrosion resistant coating Patent
Metal soldering with hydrazine monoperfluoro alkanoate for corrosion resistant coatings
Bauman, A. J.↗
Aerophysical plasma alleviation
Reentry plasma sheath alleviation by injecting sulfur hexafluoride or hydrazine into boundary layer
Parmentier, E. M.↗
Hybrid resistojet development Final report
High specific impulse of several hydrazine thrustors ignited by electrical heaters within thrust chamber during experimental evaluation
Source record↗
Planetary explorer liquid propulsion study Final report, Jul. 1970 - Jan. 1971
Evaluation of Planetary Explorer propulsion systems of monopropellant hydrazine type for use on Venus mission satellite
Mc Cabe, J. E.↗
Comment on 'Preignition products from propellants at simulated high altitude conditions'
Engine pressure spiking restart preignition products, determining hydrazine nitrate and dinitrate presence by spectrum analysis
Dauerman, L.↗
Thymine - A possible prebiotic synthesis
Possible prebiotic synthesis of thymine by heating uracil, paraformaldehyde and hydrazine in ammoniacal solution for three days at 70 C
Kimball, A. P.↗
Propellant-powered actuator for gas generators
Hydrazine operated monopropellant generators are used for spacecraft rocket engines and propellant pressurization systems. Measured work output of monopropellant actuators compares favorably with output of squib-type actuators.
Makowski, M. J.↗
TOPS attitude propulsion subsystem technology
The thermoelectric outer-planet spacecraft (TOPS) attitude propulsion subsystem effort is summarized. It includes the tradeoff rationale that went into the selection of anhydrous hydrazine as the propellant, and a brief description of three types of 0.445-N (100-mlbf) thrusters that were purchased for in-house evaluation. A discussion is also included of the 0.2224-N (50-mlbf)-developed thrusters and their integration with a portable, completely enclosed, propulsion module that was designed and developed to support the TOPS single-axis attitude control tests in the celestarium.
Moynihan, P. I.↗