Resin systems investigated for improving ablative materials for use with fluorine-containing liquid propellant system
Protective coating of phosphate-bonded zirconia for regeneratively cooled thrust chamber
Improve method for Apollo propellant system decontamination and propellant tank dryin
Critical experiments and nuclear analyses of tungsten water moderated nuclear rocket reacto
Preparation, and evaluation of polyimide sulfone resins, graphite-silica reinforced polyamide resins...
Low cost graphite powder and phenolic resin molding compounds for use in rocket engine nozzle
Reaction kinetics ablation program to predict ablation performance of rocket nozzle heat protection ...
Techniques for rating performance of ablative materials in liquid-propellant rocket engine
Evaluating low cost ablative materials for use in large solid propellant rocket motor
Heat transfer, altitude performance, and combustion efficiency evaluated in study of space storable ...
Twist-flex life, tensile properties, thermal expansion coefficient, and permeabilty of polymeric mat...
Interlaminar-shear testing of resin-filament wound composite materials for cryogenic us
Annotated abstracts of materials science technical memorandum - plastic, composite, explosive, lubri...
Materials for potassium lubricated journal bearing and shaft applications in high temperature space ...
Liquid and gaseous oxygen difluoride compatibility tests with plastic and metal orifices and metal i...
Alternating current circuit breakers and direct current engine contactors for space nuclear electric...
Protective coating of phosphate-bonded zirconia for regeneratively cooled thrust chamber
Improve method for Apollo propellant system decontamination and propellant tank dryin
Critical experiments and nuclear analyses of tungsten water moderated nuclear rocket reacto
Preparation, and evaluation of polyimide sulfone resins, graphite-silica reinforced polyamide resins...
Low cost graphite powder and phenolic resin molding compounds for use in rocket engine nozzle
Reaction kinetics ablation program to predict ablation performance of rocket nozzle heat protection ...
Techniques for rating performance of ablative materials in liquid-propellant rocket engine
Evaluating low cost ablative materials for use in large solid propellant rocket motor
Heat transfer, altitude performance, and combustion efficiency evaluated in study of space storable ...
Twist-flex life, tensile properties, thermal expansion coefficient, and permeabilty of polymeric mat...
Interlaminar-shear testing of resin-filament wound composite materials for cryogenic us
Annotated abstracts of materials science technical memorandum - plastic, composite, explosive, lubri...
Materials for potassium lubricated journal bearing and shaft applications in high temperature space ...
Liquid and gaseous oxygen difluoride compatibility tests with plastic and metal orifices and metal i...
Alternating current circuit breakers and direct current engine contactors for space nuclear electric...
Protective coating of phosphate-bonded zirconia for regeneratively cooled thrust chamber
Improve method for Apollo propellant system decontamination and propellant tank dryin
Critical experiments and nuclear analyses of tungsten water moderated nuclear rocket reacto