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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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Computer program development for charring ablative materials, chemically reacting laminar boundary layers, and turbulent boundary layer initiation
Thermal and mechanical properties of phenolic nylon ablation materials
Ablative materials examination before and after test firing
Ablation product absorption and line transitions effects on shock layer radiative transport around blunt body
Investigation of low density ablative materials for heat shields on reentry vehicles
Simulated charring ablator performance during reentry phase
Ablation behavior of heat shield of Apollo command module over wide range of thermal environments
Ablative effectiveness of low density phenolic nylon materials
Design of injectors and ablative thrust chambers for FLOX propane rocket engine with 1.2 inch throat diameter
Throat and nozzle insert design for ablative rocket engine using storable propellants
Chemical equilibrium of ablation materials including condensed species
Design, development, and testing of 1000 pound thrust FLOX-propane ablative rocket engine
Chemical analysis of ablative materials
Upwash patterns on ablating and nonablating cones at hypersonic speeds
Thermochemical data from simulated pyrolysis gas flow through ablating char layer
Sensor device with switches for measuring surface recession of charring and noncharring ablators
Numerical analysis of restrained shrinkage stresses in ablation heat shields
Ablative heat shield materials for Mars and Venus atmospheric entries