Flight investigation of the effects of Apollo heat-shield singularities on ablator performance
Launch vehicle flight tests of effects of Apollo heat shield irregularities on ablative material performance
Ohare, B. 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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A study of the reaction-plane approximation in ablation analyses
Chemical reaction-plane approximation in ablation analyses
Stroud, C. W.↗
Low-density, leading-edge bluntness, and ablation effects on wedge-induced laminar boundary layer separation at moderate enthalpies in hypersonic flow
Low density, leading edge bluntness, and ablation effects on wedge induced laminar boundary layer separation at moderate enthalpies in hypersonic flow
Anders, J. B.↗
Surface Effects Resulting from Tektite Ablation
Photographic results of surface effects caused by tektite ablation
Blackledge, M. L.↗
Measurements of the total surface emittance of charring ablators.
Total normal emittance measurements of charred ablator surfaces, discussing gas cap radiation effect
Pope, R. B.↗
Calculation of temperature profile in ablator char using MIMIC.
Differential equation of temperature profile in carbon zone of ablator simulated using digital- analog simulator language /MIMIC/
April, G. C.↗
A study of the effects of environmental and ablator performance uncertainties on heat shielding requirements for blunt and slender hyperbolic-entry vehicles.
Environmental and ablator performance uncertainties effects on heat shielding requirements for blunt and slender hyperbolic entry vehicles
Coleman, W. D.↗
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.↗
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.↗