Apollo lunar module descent engine ablative chamber - Injector compatibility improvement study Summary report
Summary of material and design improvements to reduce ablative chamber throat erosion in lunar module descent engine
Maucieri, J. J.↗
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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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Experimental study of groove patterns on ablated surfaces in the Langley 8-foot high- temperature structures tunnel
Grove patterns on ablated surfaces of Teflon 8-foot high temperature structures tunnel
Bruce, W. E., Jr.↗
Investigation of effects of ablative discrepancies on nozzle performance reliability Final report
Effects of ablative discrepancies on nozzle performance reliability
Warga, J. J.↗
Formulation, derivation and development of the analysis of the interaction of ablating protection systems and stagnation region heating
Conservation equations for analysis of interaction of ablating protection systems and stagnation region heating
Engel, C. D.↗
Apollo lunar module descent engine ablative chamber-injector compatibility improvement study. Torch test materials evaluation
Injector compatibility improvement for Apollo lunar module descent engine ablative chamber
Source record↗
Project Apollo evaluation of ablation heat shield material specimens incorporating electrical connectors, phase 1
Evaluation of ablation heat shield material incorporating electrical connectors
Gunderson, R. T.↗
Evaluation of the energy transfer in the char zone during ablation. Part 1 - Theoretical and experimental results for heat shield surface temperatures up to 3000 F Final report
Energy transfer in pyrolysis product flow through char layer of nylon phenolic resin ablator
April, G. C.↗
An analysis of a charring ablation thermal protection system
Computer program for predicting charring ablation performance of heat shielding
Curry, D. M.↗
Apollo ablator thermal performance at superorbital entry velocities
Apollo ablator thermal performance at superorbital entry velocities
Curry, D. M.↗
Advanced methods for calculating radiation transport in ablation-product contaminated boundary layers
Prediction method for calculating radiation transport in ablation product contaminated, hypersonic boundary layers
Nicolet, W. E.↗
Investigation of char formation and surface recession of a composite ablation material with a silicone-resin base
Char formation and surface recession of composite ablation material with silicone resin base
Mc Lain, A. G.↗
A coupled computer code for the transient thermal response and ablation of non-charring heat shields and nose tips
Coupled computer code for transient thermal response and ablation of noncharring heat shields and nose tips
Anderson, L. W.↗
Transpirationally cooled heat ablation system Patent
Transpirationally cooled heat ablation system for interplanetary spacecraft reentry shielding
Downs, W. R.↗
Hypersonic boundary-layer transition on ablating and nonablating cones
Ablation effects on transition Reynolds number of hypersonic boundary layer on slender cones
Fischer, M. C.↗
Application of photographic pyrometry to ablation models
Photographic pyrometry for surface temperature measurements on ablation models, discussing technique accuracy and limitations
Exton, R. J.↗
Spectral and integrated emittance of ablation chars and carbon
Ablation chars, carbon and graphite spectral emittance and reflectance as function of wavelength and temperature, noting applications to atmospheric entry heat shielding
Spitzer, C. R.↗
Particle removal in the ablation of artificial graphite
Particle removal in ablation of artificial graphite linked to oxidation, using high speed motion pictures in analysis
Maahs, H. G.↗