Radiation transport for blunt-body flows including the effects of lines and ablation layer, volume 3
Analyses of radiation transport for blunt bodies returning from space missions at hypersonic speed
Chin, J. H.↗
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An analysis of the coupled chemically reacting boundary layer and charring ablator. Part 3 - Nonsimilar solution of the multicomponent laminar boundary layer by an integral matrix method
Laminar boundary layer problems solved by integral matrix methods
Bartlett, E. P.↗
An analysis of the coupled chemically reacting boundary layer and charring ablator. Part 2 - Finite difference solution for the in-depth response of charring materials considering surface chemical and energy balances
Computer program for finite difference equation analysis of in-depth response of materials exposed to high temperature environment
Moyer, C. B.↗
An analysis of the coupled chemically reacting boundary layer and charring ablator. Part 4 - A unified approximation for mixture transport properties for multicomponent boundary-layer applications
Bifurcation approximation for binary and thermal diffusion coefficients, mixture viscosity, and thermal conductivity of laminar boundary layer
Bartlett, E. P.↗
An analysis of the coupled chemically reacting boundary layer and charring ablator. Part 5 - A general approach to the thermochemical solution of mixed equilibrium-nonequilibrium, homogeneous or heterogeneous systems
Computer program for solutions to equilibrium and nonequilibrium chemical state relations for open and closed thermodynamic systems
Kendall, R. M.↗
Radiation transport for stagnation flows including the effect of lines and ablation layer.
Numerical methods for radiation transport for inviscid stagnation flows, detailing spectral nature of radiation emission and absorption
Chin, J. H.↗
Experimental setup for the laboratory investigation of micrometeoroid ablation using a dust accelerator
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Evan Thomas↗
Further studies of the coupled chemically reacting boundary layer and charring ablator. Part 4 - Nonsimilar solution of an incompressible turbulent boundary layer by an integral matrix method
Nonsimilar solution of incompressible turbulent boundary layer by integral matrix method
Anderson, L. W.↗
Thermochemical ablation of rocket nozzle insert materials Final report
Resistance of rocket nozzle throat insert materials to corrosion and melting
Clark, K. J.↗
Large hydrogen-oxygen ablative chamber test program Final report
Large hydrogen-oxygen albative chamber
Kovach, R. J.↗
Method for making a heat insulating and ablative structure
Filling honeycomb matrix with deaerated paste filler
Newcombe, C. A.↗
Radiation transport for stagnation flows including effects of lines and ablation layer.
Numerical methods for radiation transport for inviscid stagnation flows, detailing spectral nature of radiation emission and absorption
Chin, J. H.↗
Apollo lunar module descent engine ablative chamber - Injector compatibility improvement study Final report
Improved liner for Apollo lunar module descent engine injection chamber
Source record↗
Development of low cost ablative nozzles for solid propellant rocket motors, volume 2 Final report
Evaluation of low cost materials for solid propellant rocket motors
Laramee, R. C.↗
An experimental study of a carbon-phenolic ablation material
Experimental ground tests of carbon-phenolic heat shield material
Sutton, K.↗
Properties of ablation and insulation materials. Volume 2 - Thermal properties of three rigidized fibrous insulators
Thermal conductivity, thermal expansion, and heat capacity determinations for three rigidized fibrous insulators - Vol. 2.
Pears, C. D.↗
A theoretical study of nose ablation
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Roberts, L.↗
Experimental ablation cooling
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Bond, A. C.↗