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.↗
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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.↗
Further studies of the coupled chemically reacting boundary layer and charring ablator. Part 1 - Summary Final report
Computer program development for charring ablative materials, chemically reacting laminar boundary layers, and turbulent boundary layer initiation
Anderson, L. W.↗
An investigation of some thermal and mechanical properties of a low-density phenolic-nylon ablation material Final report
Thermal and mechanical properties of phenolic nylon ablation materials
Pears, C. D.↗
The post-test analysis of ablative materials Final report, 11 Jul. 1967 - 15 May 1968
Ablative materials examination before and after test firing
Burrell, B. W.↗
Effect of ablation product absorption and line transitions on shock layer radiative transport
Ablation product absorption and line transitions effects on shock layer radiative transport around blunt body
Hoshizaki, H.↗
A study of the potential benefits of using lower-density ablators for protecting manned lifting-body entry vehicles
Investigation of low density ablative materials for heat shields on reentry vehicles
Moss, J. N.↗
A study of the simulation of the flight performance of charring ablators in ground facilities
Simulated charring ablator performance during reentry phase
Tompkins, S. S.↗