Low cost fabrication method for ablative heat shield panels for space shuttles
Fabrication of low cost ablative heat shield panels for space shuttles
Abbott, H. T.↗
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Method and apparatus for making a heat insulating and ablative structure Patent
Method and apparatus for fabrication of heat insulating and ablative reentry structure
King, R. W.↗
Ablation sensor Patent
Ablation sensor for measuring char layer recession rate using electric wires
Le Bel, P. J.↗
Low cost ablative heat shields for space shuttles Final report
Fabrication of prototype low density ablative heat shield panels for space shuttles with production cost estimates
Freeder, H.↗
Numerical analysis of the transient response of ablating axisymmetric bodies including the effects of shape change
Differential equations governing transient response of ablating axisymmetric orthotropic bodies and effect of shape change
Howser, L. M.↗
Artificial meteor ablation studies - Iron oxides
Artificial meteor ablation studies of natural minerals composed of magnetite and hematite
Blanchard, M. B.↗
Ablative thermal protection systems
Light weight, low cost, ablative thermal protection system for space shuttles
Pittman, C. M.↗
Ablative leading edge design concepts for the shuttle orbiter
Design of low cost ablator leading edge for space shuttle thermal protection system
Graham, J. W.↗
Development and testing of ablative rocket engine with selected 7.62-centimeter /3.0 in/ diameter throat inserts
Development and testing of ablative rocket engine with selected 7.62 cm /3.0 in./ diameter throat inserts, and testing of zirconia reinforced with tungsten-rhenium wire for throat insert material
Pavli, A. J.↗
Supersonic flow over convex and concave shapes with radiation and ablation effects
Numerical method of unsteady adjustment for calculating inviscid flow fields about convex and concave shapes on atmospheric entry with ablation
Bohachevsky, I. O.↗
Low-cost ablative heat shields for space shuttles
Low cost replaceable ablative heat shield panels for space shuttles
Chandler, H. H.↗
Development of low cost ablative nozzles for large solid propellant rocket motors
Evaluation of selected low-cost ablative materials for large solid rocket engine nozzle design
Sohl, J. D.↗
Ablative response of a silica phenolic to simulated liquid propellant rocket engine operating conditions
Ablative response of silica phenolic to simulated liquid propellant rocket engine operating conditions
Wool, M. R.↗
Computer program for the transient response of ablating axisymmetric bodies including the effects shape change
Computer program for analyzing transient response of ablating axisymmetric bodies including effects of shape change
Howser, L. M.↗
On chemical reactions in the char zone during ablation
Analysis of reacting flow of pyrolysis products through char layer of low density, nylon phenolic resin, charring ablators and porous graphite
April, G. C.↗
Modeling reacting gas flow in the char layer of an ablative heat shield during reentry
Ablative heat shield char layer, examining reacting nonequilibrium pyrolysis gas flow
April, G. C.↗
Ablative material response to CO2 laser radiation
Ablative materials performance in high radiative heat flux environments produced by CW carbon dioxide laser
Brewer, W. D.↗
An analytical model for hypersonic ablation of thoria dispersed nickel chromium alloy
Thoria dispersed Ni-Cr alloy hypersonic entry ablation model, accounting for Cr oxidation
Goldstein, H. E.↗