The effects of heat load, ablator density, and backup structure, etc. upon the heat shield performance of the lightweight phenolic carbon ablators named LATS were investigated using a one-dimensional ablation analysis code. The ablator density was assumed to be from about 260 to 1000 kg/m3. Heat flux time histories of a rectangular pattern were assumed, where cases of constant heating duration time and constant accumulated heat load (up to 600 MJ/m2) were considered. The heating level was assumed to be from 1 to 10 MW/m2, which means that the ablator surface is in the region of diffusion control oxidation/sublimation. The materials of the backup wall are assumed to be aluminum, stainless steel and high density CFRP. Main findings are: (1) F...
This paper presents the development of the light weight Phenolic Impregnated Carbon Ablators (PICA) ...
High heat flux is encountered in space applications in re-entry flight at the thermal protection sys...
The primary physical response phenomena associated with ablative insulators are discussed in this pr...
The effects of density, thickness and heat load upon the heat shield performance of the lightweight ...
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...
The TPS (Thermal Protection System) is a subsystem providing protection and isolation from aerodynam...
Ablative thermal protection materials are a key technology for current and future space exploration ...
A new class of lightweight carbon fiber reinforced plastic (CFRP)–-the lightweight ablator series fo...
Surface ablation and in-depth temperature distribution of the charring material are the key properti...
A critical problem in the design of Thermal Protection Systems (TPS) for planetary probes and re-ent...
The Thermal Protection System (TPS) protects (insulates) a body from the severe heating encountered ...
A comprehensive analysis of publicly available research statements on spallation processes of ablati...
Influence of environmental conditions on thermal performance of low density charring ablato
A lightweight carbon-phenolic ablator, with a density of 0.5 g/cm3, designed to be used as a thermal...
This paper presents the development of the light weight Phenolic Impregnated Carbon Ablators (PICA) ...
High heat flux is encountered in space applications in re-entry flight at the thermal protection sys...
The primary physical response phenomena associated with ablative insulators are discussed in this pr...
The effects of density, thickness and heat load upon the heat shield performance of the lightweight ...
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...
The TPS (Thermal Protection System) is a subsystem providing protection and isolation from aerodynam...
Ablative thermal protection materials are a key technology for current and future space exploration ...
A new class of lightweight carbon fiber reinforced plastic (CFRP)–-the lightweight ablator series fo...
Surface ablation and in-depth temperature distribution of the charring material are the key properti...
A critical problem in the design of Thermal Protection Systems (TPS) for planetary probes and re-ent...
The Thermal Protection System (TPS) protects (insulates) a body from the severe heating encountered ...
A comprehensive analysis of publicly available research statements on spallation processes of ablati...
Influence of environmental conditions on thermal performance of low density charring ablato
A lightweight carbon-phenolic ablator, with a density of 0.5 g/cm3, designed to be used as a thermal...
This paper presents the development of the light weight Phenolic Impregnated Carbon Ablators (PICA) ...
High heat flux is encountered in space applications in re-entry flight at the thermal protection sys...
The primary physical response phenomena associated with ablative insulators are discussed in this pr...