AN ENGINEERING ANALYSIS OF THE WEIGHTS OF ABLATING SYSTEMS FOR MANNED REENTRY VEHICLES
Explore the source record for details and available documents.
Swann, R. T.↗
SEARCH · Engineering Papers
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.
Quote a phrase for an exact phrase match. Source license links do not imply unrestricted reuse.
Cinefluorography of small ablative thrust chambers during hot firing.
X-ray image intensifier in conjunction with motion picture film sequencing of thrust chamber image during hot firing to obtain failure analysis data
CINEFLUOROGRAPHY↗
A multicomponent boundary layer chemically coupled to an ablating surface.
Incident of severe low level turbulence in clear air
CLEAR AIR TURBULENCE↗
A general study of the dynamics and stability of ablative melt layers progress report, 1 apr. - 30 sep. 1965
Explore the source record for details and available documents.
Source record↗
Investigation of resin systems for improved ablative materials Interim report, 10 Jan. - 1 Jul. 1966
Preparation, and evaluation of polyimide sulfone resins, graphite-silica reinforced polyamide resins, and resin resistance to FLOX- methane, and fluorine-hydrogen fuels
Burns, E. A.↗
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.↗
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
Explore the source record for details and available documents.
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↗