A study of artificial meteors as ablators.
Simulated meteor ablation tests using artificial meteors of gabbro, basalt and steel in ultrahigh enthalpy plasma jet
Shepard, C. E.↗
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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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Visible and near-infrared emittance of ablation chars and carbon.
Visible and near IR spectral reflectance and emittance at high temperature of ablation chars, carbon and graphite
Spitzer, C. R.↗
The effect of oxygen depletion in gas-phase chemical reactions on the 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.↗
Structural synthesis of an ablating thermostructural panel.
Structural synthesis for ablating thermostructural panels in planetary entry environment
Schmit, L. A., Jr.↗
Ablation testing in ballistic ranges.
Ballistic range applications to ablation effects on cone aerodynamic characteristics
Intrieri, P. F.↗
Performance of charring ablative materials in the diffusion-controlled surface combustion regime.
Ablative behavior of low and high density phenolic nylon in diffusion controlled surface combustion regime
Dickey, R. R.↗
Linearized theory of radiative heat transfer for ablating bodies at meteoric speeds.
Linearized radiative heat transfer theory for ablating bodies flying in earth atmosphere at meteoric speeds
Yoshikawa, K. K.↗
Convective and radiative heat transfer to an ablating body.
Convective and radiative heat transfer to reentry vehicles protected by ablation heat shields
Hoshizaki, H.↗
Ablative surface recession and mass loss on large-angle sphere-cones.
Approximate method to predict ablative recession rate and mass loss on sphere cones in Martian atmosphere entry
Orlik-Rueckemann, K. J.↗
Effects of environmental and ablator performance uncertainties on heat-shielding requirements for hyperbolic entry vehicles.
Environmental and ablator performance uncertainties effects on heat shielding requirements for blunt and slender hyperbolic entry vehicles
Coleman, W. D.↗
Orderly three-dimensional processes in turbulent boundary layers on ablating bodies
Orderly three dimensional processes in turbulent boundary layers on biconic, concave, and convex ablating bodies in Mach 7 airstream
Canning, T. N.↗
Charring ablation performance in turbulent flow. Volume 1 - Analytical and experimental studies
Semiempirical correlation techniques for predicting charring ablation performance of Apollo heat shield in turbulent flow
Crowder, P. A.↗
Charring ablation performance in turbulent flow. Volume 2 - Computer program
FORTRAN 4 program for predicting charring ablation performance of Apollo heat shield in turbulent flow
Colony, R.↗
Radiofrequency transmission characteristics of several ablation materials
Transmission loss and effects on antenna radiation patterns and impedance produced by thermally degraded ablation materials
Castellow, S. L., Jr.↗
Radiofrequency transmission characteristics of candidate ablation materials for planetary-entry-vehicle heat shields
Radio frequency transmission characteristics of ablation materials for planetary entry vehicle heat shields
Chapman, A. J.↗
Comparative evaluation of ablating materials in arc plasma jets
Comparative evaluation of ablative materials in arc plasma jets
Clark, C. F.↗
The structural synthesis of an ablating thermostructural panel
Transient thermal analysis and structural analysis for synthesis of ablating thermostructural panels in planetary entry environment
Schmit, L. A., Jr.↗
Multidimensional gas flow through permeable char layers and its effects on ablation
Pressure fields and multidimensional gas flow in permeable char layers and effects on ablation
Bush, H. G.↗