Low-density carbon/phenolic is a class of ablative materials that is attractive for space exploration missions that use blunt bodies where weight and performance of the material are of primary importance, but shape preservation is not critical. Phenolic Impregnated Ceramic Ablator (PICA) is a material of this family develop by NASA for high-speed atmospheric entry mission
Future space exploration missions beyond Earth's orbit, such as sample returns from Mars, will use a...
Phenolic Impregnated Carbon Ablator (PICA) was invented in the mid 1990's and due to its relatively ...
Protecting a spacecraft during atmospheric entry is one of highest risk factors that needs to be mit...
Low-density carbon/phenolic is a class of ablative materials that is attractive for blunt body space...
A space vehicle which undergoes the atmospheric re-entry or a planetary entry needs the heat shield ...
This paper presents the development of the light weight Phenolic Impregnated Carbon Ablators (PICA) ...
The initial temperature response of phenolic injected carbon ablators (PICA) under arcjet test condi...
Phenolic Impregnated Carbon Ablator (PICA) is a low-density ablator that has been used as the planet...
A critical problem in the design of Thermal Protection Systems (TPS) for planetary probes and re-ent...
International audienceSpacecrafts such as Stardust (NASA, 2006) are protected by an ablative Thermal...
Ablative thermal protection materials are a key technology for current and future space exploration ...
Carbon-phenolic ablative materials represent the most effective solution as thermal shield for a bro...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/83619/1/AIAA-2010-1175-298.pd
A lightweight carbon-phenolic ablator, with a density of 0.5 g/cm3, designed to be used as a thermal...
peer reviewedHigh-fidelity models have been developed in the recent years to predict the response of...
Future space exploration missions beyond Earth's orbit, such as sample returns from Mars, will use a...
Phenolic Impregnated Carbon Ablator (PICA) was invented in the mid 1990's and due to its relatively ...
Protecting a spacecraft during atmospheric entry is one of highest risk factors that needs to be mit...
Low-density carbon/phenolic is a class of ablative materials that is attractive for blunt body space...
A space vehicle which undergoes the atmospheric re-entry or a planetary entry needs the heat shield ...
This paper presents the development of the light weight Phenolic Impregnated Carbon Ablators (PICA) ...
The initial temperature response of phenolic injected carbon ablators (PICA) under arcjet test condi...
Phenolic Impregnated Carbon Ablator (PICA) is a low-density ablator that has been used as the planet...
A critical problem in the design of Thermal Protection Systems (TPS) for planetary probes and re-ent...
International audienceSpacecrafts such as Stardust (NASA, 2006) are protected by an ablative Thermal...
Ablative thermal protection materials are a key technology for current and future space exploration ...
Carbon-phenolic ablative materials represent the most effective solution as thermal shield for a bro...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/83619/1/AIAA-2010-1175-298.pd
A lightweight carbon-phenolic ablator, with a density of 0.5 g/cm3, designed to be used as a thermal...
peer reviewedHigh-fidelity models have been developed in the recent years to predict the response of...
Future space exploration missions beyond Earth's orbit, such as sample returns from Mars, will use a...
Phenolic Impregnated Carbon Ablator (PICA) was invented in the mid 1990's and due to its relatively ...
Protecting a spacecraft during atmospheric entry is one of highest risk factors that needs to be mit...