Project Apollo evaluation of ablation heat shield material specimens incorporating electrical connectors, phase 1
Evaluation of ablation heat shield material incorporating electrical connectors
SEARCH · Engineering Papers
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.
Quote a phrase for an exact phrase match. Source license links do not imply unrestricted reuse.
Evaluation of ablation heat shield material incorporating electrical connectors
Energy transfer in pyrolysis product flow through char layer of nylon phenolic resin ablator
Computer program for predicting charring ablation performance of heat shielding
Apollo ablator thermal performance at superorbital entry velocities
Prediction method for calculating radiation transport in ablation product contaminated, hypersonic boundary layers
Char formation and surface recession of composite ablation material with silicone resin base
Coupled computer code for transient thermal response and ablation of noncharring heat shields and nose tips
Transpirationally cooled heat ablation system for interplanetary spacecraft reentry shielding
Ablation effects on transition Reynolds number of hypersonic boundary layer on slender cones
Photographic pyrometry for surface temperature measurements on ablation models, discussing technique accuracy and limitations
Ablation chars, carbon and graphite spectral emittance and reflectance as function of wavelength and temperature, noting applications to atmospheric entry heat shielding
Particle removal in ablation of artificial graphite linked to oxidation, using high speed motion pictures in analysis
Melting ablation for two dimensional and axisymmetric blunt bodies with body force, predicting gas-liquid interface temperature for free stream conditions
Viscous radiating flowfield coupled with ablation for computations on blunt body entering earth atmosphere at interplanetary return velocities
Ablation of heat shielding materials subjected to superorbital reentry conditions, noting dependence on heating rate to surface
Faint meteor ablation processes, presenting evidence of solid consistency prior to atmospheric entry, vaporization, wake blending and trails
Ablative materials for thermal protection at low convective heating rates, comparing foam and state-of-art materials performance