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.↗
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Results for “Ablative”
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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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.↗
Ablative characterization of seven heat shield materials - A review of the NASA-SRI Round-Robin program.
Ablation characteristics of heat shield materials measured in arc heated wind tunnels, considering influence of model scale, heating rate and pressure level
Clark, C. F.↗
Performance of various ablative materials in a large hydrogen/oxygen thrust chamber.
Ablative materials in hydrogen/oxygen thrust chamber using expansion nozzle to substitute regenerative thrust chamber assembly
Kovach, R. J.↗
Ablative thermal protection at low heating rates.
Ablative materials thermal protection characteristics at low heating rates evaluated by convective heating tests, stressing polyurethane foam composite
Goldstein, H. E.↗
Dielectric processing for low-cost ablation heat shields.
Ablation heat shields, emphasizing dielectric low cost fabrication and application to entry vehicles
King, C. B.↗
Flash X-ray technique for recession measurements in ablating models.
Flash X ray unit with special film transport devices to obtain sequenced dynamic radiographs of ablating models during reentry simulation tests
Kassel, P. C., Jr.↗