Application of the line-source technique for vacuum thermal conductivity measurements.
Line source technique for ablative heat shield materials thermal conductivity measurements, comparing vacuum and atmospheric test results
Comparin, R. A.↗
SEARCH · Search NASA
Results for “Heat Shield”
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.
Simulation of Venus atmospheric entry by earth re-entry.
Atmospheric gas composition effects on shock layer radiative heat transfer and heat shield response in Venus entry simulated by earth reentry
Spiegel, J. M.↗
Hypersonic cruise vehicle wing structure evaluation - Volume 2, sections 11-22
Structure size, weight, flutter, fatigue, creep, and heat shield analyses for hypersonic cruise vehicle wing
Davis, G. W.↗
An analysis of a charring ablation thermal protection system
Computer program for predicting charring ablation performance of heat shielding
Curry, D. M.↗
An experimental study of a carbon-phenolic ablation material
Experimental ground tests of carbon-phenolic heat shield material
Sutton, K.↗
Hypersonic reentry vehicle Patent
Aerodynamic configuration of reentry vehicle heat shield to provide longitudinal and directional stability at hypersonic velocities
Lamb, R. H.↗
Atmospheric entry into Jupiter
Blunt and conical body optimum heat shield shapes for Jupiter atmospheric entry, noting shallow flight path
Tauber, M. E.↗
Tailoring polymers for entry into the atmospheres of Mars and Venus
Polymers development for ablative heat shields, aeroshell structures, antennas, insulators, electronic packaging, etc, to meet Mars and Venus atmospheric entry requirements
Nagler, R. G.↗
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.↗
Massive blowing effects on viscous, radiating, stagnation-point flow
Massive blowing effect on stagnation point radiative energy transfer of ablative heat shield during planetary entry at hypersonic velocities
Wilson, K. H.↗
Application of the line-source technique for vacuum thermal conductivity measurements
Line source technique for ablative heat shield materials thermal conductivity measurements, comparing vacuum and atmospheric test results
Comparin, R. A.↗
Reentry capsule dynamics
Blunt heat shield effectiveness for trailing payload in reentry capsules, discussing dynamic instability effect
Ericsson, L. E.↗
Heating environment and protection during Jupiter entry
Environmental heat shielding for various sized Jupiter atmospheric entry probes
Tauber, M. E.↗
Azine polymers and process for preparing the same Patent
Synthesis of azine polymers for heat shields by azine-aromatic aldehyde reaction
Dalelio, G. F.↗
Synthesis of polymeric schiff bases by reaction of acetals and amine compounds Patent
Synthesis of schiff bases for heat shields by acetal amine reactions
Dalelio, G. F.↗
Experimental evaluation of a purged substrate multilayer insulation system for liquid hydrogen tankage
Thermal cycling tests of ground and space liquid hydrogen storage tank heat shielding with multilayer, purged substrate, thermal insulation blankets
De Witt, R. L.↗
Spacecraft Patent
Design and development of spacecraft with outer shell structure heat shielding and built-in, removable excursion module
Vanalstyne, E. M.↗
An analysis of predicted space shuttle temperatures and their impact on thermal protection systems
Comparison of space shuttle aerodynamic heating analyses for metallic heat shield and surface insulation concepts
Forney, J. A.↗