The effects of density, thickness and heat load upon the heat shield performance of the lightweight phenolic carbon ablators named LATS (Lightweight Ablator series for Transfer vehicle Systems) were examined quantitatively for both arc-heated test and re-entry heating conditions using a one-dimensional ablation analysis code. Thermal conductivity values of the ablator were tuned based on the arc-heated test results by matching the calculated temperatures to the measured data. Main findings are: (1) For both heating conditions, the heat shielding performance of the ablator has the same tendencies with respect to parameters of the ablator density, thickness and heat load. (2) The dependency of the back surface temperature upon the ablator den...
A comprehensive analysis of publicly available research statements on spallation processes of ablati...
Abstract Space exploration missions rely on ablative heat shields for the thermal protection of spac...
Coking phenomenon for low density carbon-phenolic ablative material exposed to aerodynamic heating i...
The effects of heat load, ablator density, and backup structure, etc. upon the heat shield performan...
A space vehicle which undergoes the atmospheric re-entry or a planetary entry needs the heat shield ...
For protecting the spacecraft against the severe heating during the atmospheric reentry, the ablativ...
Surface ablation and in-depth temperature distribution of the charring material are the key properti...
Adequately characterizing the ablative Thermal Protection System (TPS) of an entry vehicle is critic...
A new class of lightweight carbon fiber reinforced plastic (CFRP)–-the lightweight ablator series fo...
A lightweight carbon-phenolic ablator, with a density of 0.5 g/cm3, designed to be used as a thermal...
Ablative thermal protection materials are a key technology for current and future space exploration ...
The TPS (Thermal Protection System) is a subsystem providing protection and isolation from aerodynam...
Influence of environmental conditions on thermal performance of low density charring ablato
Several types of anomalous behavior have been observed with phenolic based ablatives in post-fired n...
Low-density carbon/phenolic is a class of ablative materials that is attractive for blunt body space...
A comprehensive analysis of publicly available research statements on spallation processes of ablati...
Abstract Space exploration missions rely on ablative heat shields for the thermal protection of spac...
Coking phenomenon for low density carbon-phenolic ablative material exposed to aerodynamic heating i...
The effects of heat load, ablator density, and backup structure, etc. upon the heat shield performan...
A space vehicle which undergoes the atmospheric re-entry or a planetary entry needs the heat shield ...
For protecting the spacecraft against the severe heating during the atmospheric reentry, the ablativ...
Surface ablation and in-depth temperature distribution of the charring material are the key properti...
Adequately characterizing the ablative Thermal Protection System (TPS) of an entry vehicle is critic...
A new class of lightweight carbon fiber reinforced plastic (CFRP)–-the lightweight ablator series fo...
A lightweight carbon-phenolic ablator, with a density of 0.5 g/cm3, designed to be used as a thermal...
Ablative thermal protection materials are a key technology for current and future space exploration ...
The TPS (Thermal Protection System) is a subsystem providing protection and isolation from aerodynam...
Influence of environmental conditions on thermal performance of low density charring ablato
Several types of anomalous behavior have been observed with phenolic based ablatives in post-fired n...
Low-density carbon/phenolic is a class of ablative materials that is attractive for blunt body space...
A comprehensive analysis of publicly available research statements on spallation processes of ablati...
Abstract Space exploration missions rely on ablative heat shields for the thermal protection of spac...
Coking phenomenon for low density carbon-phenolic ablative material exposed to aerodynamic heating i...