Chamber technology for space storable propellants Final report, Jun. 1964 - Sep. 1969
Chamber technology for space storable propellant combinations featuring oxygen difluoride
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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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Space storable propellant vacuum performance evaluation Final report
Rocket engine tests using space storable propellants and various injector configurations
Waldman, B. J.↗
Experimental evaluation of 7.82-inch /19.8-cm/ diameter throat inserts in a storable-propellant rocket engine
Failure mechanisms for specific materials and design concepts for storable propellant rocket engines
Peterson, D. A.↗
Treatment of metal surfaces for use with space storable propellants - A critical survey
Treatment of metallic surfaces for use with space storable propellants
Muraca, R. F.↗
Analytical evaluation of space storable propellants for unmanned Jupiter and Saturn orbiter missions
Analytical evaluation of space storable propellants for unmanned Jupiter and Saturn orbiter missions
Oglebay, J. C.↗
System analysis of gelled space-storable propellants Final report, Jun. 1969 - May 1970
System analysis of gelled space storable propellants
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Task 3 space storable propellant module environmental control technology Summary report
Thermal control system for space storable propellant module
De Land, R. E.↗
Evaluation of storable propellant reforming for use in emergency life support system design
Evaluation of storable propellants as sources of H2, O2, potable H2O, and heat for use in emergency life support system
Wright, L. O.↗
Expansion of simulated storable propellants in a supersonic nozzle.
Hydrogen and methane combustion to simulate expansion of storable propellants
Friedman, R.↗
System analysis of gelled space storable propellants
Gelled space-storable oxygen difluoride and diborane analysis, including particle preparation, yield stresses, viscosities and storability
Cabeal, J. A.↗
Experimental evaluation of several advanced ablative materials as nozzle sections of a storable-propellant rocket engine
Relative erosion resistance of ablative materials for nozzle sections of storable-propellant rocket engine
Pavli, A. J.↗
Investigation of space storable propellant acquisition devices. Volume 1 - Evaluation Final report, 24 Jul. 1969 - 15 Apr. 1970
Space storable propellant acquisition, pressurization, and tankage propulsion subsystems for Mars and Grand Tour missions
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Expulsion of storable propellants utilizing a volatile liquid as the pressurizing medium.
Volatile liquid pressurization as expulsion method for storable propellants noting in-flight refueling system design parameters
THERMODYNAMIC PROPERTY↗
Investigation of the formation and behavior of clogging material in earth and space storable propellants Final report, 9 Oct. 1968 - 9 Nov. 1969
Gel clogging material in earth and space storable propellants
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Gas-liquid space storable propellant performance Final report
Design criteria for high performance coaxial injector using gas-liquid space storable propellants
Carter, W. A.↗
Engineering model test plan. Space storable propellant module environmental control technology
Test program for engineering model of thermal control system of space storable propellant module in simulated environments
Haroldsen, O. O.↗
Advanced injectors for space storable propellants Quarterly report, 1 Oct. 1968 - 1 Jan. 1969
Fabrication and flow evaluation of injectors for space storable propellants
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Space shuttle seal material and design development for earth storable propellant systems
The results of a program to investigate and characterize seal materials suitable for space shuttle storable propellant systems are given. Two new elastomeric materials were identified as being potentially superior to existing state-of-the art materials for specific sealing applications. These materials were AF-E-124D and AF-E-411. AF-E-124D is a cured perfluorinated polymer suitable for use with dinitrogen tetroxide oxidizer, and hydrazine base fuels. AF-E-411 is an ethylene propylene terpolymer material for hydrazine base fuel service. Data are presented relative to low and high temperature characteristics as well as propellant exposure effects. Types of data included are: mechanical properties, stress strain curves, friction and wear characteristics, compression set and permeability. Sealing tests with a flat poppet-seal valve were conducted for verification of sealing capability. A bibliography includes over 200 references relating to seal design or materials and presents a concise tabulation of the more useful seal design data sources.
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