An Investigation of Ablation Behavior of Avcoat 5026-39/M over a Wide Range of Thermal Environments
Ablation behavior of heat shield of Apollo command module over wide range of thermal environments
Crouch, R. K.↗
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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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A study of the performance of low-density phenolic-nylon ablators
Ablative effectiveness of low density phenolic nylon materials
Howell, W. E.↗
Design of injectors and ablative thrust chambers for a flox-propane rocket engine with a 1.2-inch throat diameter
Design of injectors and ablative thrust chambers for FLOX propane rocket engine with 1.2 inch throat diameter
Pavli, A. J.↗
Development of Improved Throat Inserts for Ablative Rocket Engines
Throat and nozzle insert design for ablative rocket engine using storable propellants
Winter, Jerry M.↗
Chemical equilibrium of ablation materials including condensed species
Chemical equilibrium of ablation materials including condensed species
Brinkley, K. L.↗
Design, development, and testing of a 1000 pound /4450 N/ thrust FLOX-propane ablative rocket engine
Design, development, and testing of 1000 pound thrust FLOX-propane ablative rocket engine
Pauli, A. J.↗
Determination of the density and chemical profiles of government-furnished charred elastomeric ablator models
Chemical analysis of ablative materials
Source record↗
Upwash patterns on ablating and nonablating cones at hypersonic speeds
Upwash patterns on ablating and nonablating cones at hypersonic speeds
Mc Devitt, J. B.↗
Simulation of pyrolysis-gas flow through a char layer during ablation
Thermochemical data from simulated pyrolysis gas flow through ablating char layer
Clark, R. K.↗
Ablation sensor
Sensor device with switches for measuring surface recession of charring and noncharring ablators
Gurtler, C. A.↗
A numerical analysis of restrained shrinkage stresses in ablation heat shields
Numerical analysis of restrained shrinkage stresses in ablation heat shields
Dow, M. B.↗
Ablative heat shields for planetary entry vehicles.
Ablative heat shield materials for Mars and Venus atmospheric entries
Sparhawk, H. E.↗
Entry vehicle instrumentation for heat shield ablation measurements.
Make wire, light pipe and spring wire ablation sensors development for measuring parameters of heat shield materials for reentry vehicles
Lebel, P. J.↗
Evaluation of a polyurethane foam for ablative protection at low heating rates.
Low density polyurethane foam with and without honeycomb as ablative material for reentry vehicles, discussing oxidation resistance
Parker, J. A.↗
Comparison of the performance of a charring ablator under transient and constant combined convective and radiative heating.
Charring phenolic nylon ablator material pyrolysis and surface recession for cyclic and constant combined convective and radiative heating
Lundell, J. H.↗
Low temperature simulation of hypersonic melting ablation and the observed wave patterns.
Low temperature simulation of hypersonic melting ablation and wave patterns of gas-liquid interface
Chen, C.-J.↗
An evaluation of ablation mechanisms for the Apollo heat shield material.
Thermochemical and mechanical ablation mechanisms for Apollo heat shield material, comparing surface thermochemistry computer program and arc plasma tunnel data
Anderson, L. W.↗
Effects of pyrolysis-gas chemical reactions on surface recession of charring ablators.
Oxygen depletion effect in chemical reactions between pyrolysis gases and air stream on surface recession of charring ablators
Dickey, R. R.↗