Low cost ablative heat shield for space shuttles Final report, Apr. - Nov. 1970
Low cost, ablative heat shield for space shuttles
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Results for “ABLATION”
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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Ablation performance of glasslike carbons, pyrolytic graphite, and artificial graphite in the stagnation pressure range 0.035 to 15 atmospheres
Ablation performance of glasslike carbons, pyrolytic graphite, and artificial graphite in stagnation pressure range 0.035 to 15 atm
Maahs, H. G.↗
Ablation structures Patent
Design, development, and characteristics of ablation structures
Meyer, A. J., Jr.↗
Ablative performance of various low-density elastomeric composites
Performance of low density silicone-phenolic and commercial ablative composites
Howell, W. E.↗
Determination of the effects of liquid injectants on nozzle ablative performance Final report
Evaluating effect of liquid fuel injectants on ablative performance of low cost nozzle materials
Le Febvre, C. A.↗
Low cost ablative heat shields for space shuttles
Development of low cost ablative heat shields for space shuttles
Cecka, A. M.↗
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.↗
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.↗