Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/76661/1/AIAA-2005-2301-410.pd
The objective of this work has been to develop more efficient, lighter weight, and higher temperatur...
The major material and design challenges associated with the orbiter thermal protection system (TPS)...
During its lifetime a space launcher is subjected to extreme heat loads. These can dramatically infl...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/77124/1/AIAA-2006-2212-827.pd
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/77166/1/AIAA-2007-2272-508.pd
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/76198/1/AIAA-2006-7951-158.pd
Thermomechanical analysis of the space shuttle tile thermal protection system (TPS) subjected to dam...
Research on the effects of damage on the thermomechanical performance and structural integrity of th...
At the end of Space Shuttle mission, it re-enters the earth\u27s atmosphere with a speed that exceed...
Thermal protection materials and systems (TPS) are used to protect space vehicles from the heat expe...
The reusable surface insulation (RSI) material used in the shuttle thermal protection system is susc...
The characteristics and development of a lightweight reusable thermal protection system for the spac...
The TPS (Thermal Protection System) is a subsystem providing protection and isolation from aerodynam...
Thermal protection systems for hypersonic vehicles are low- to zero-fault-tolerant. In order to unde...
Spacecraft entering a planetary atmosphere require a very sophisticated thermal protection system. T...
The objective of this work has been to develop more efficient, lighter weight, and higher temperatur...
The major material and design challenges associated with the orbiter thermal protection system (TPS)...
During its lifetime a space launcher is subjected to extreme heat loads. These can dramatically infl...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/77124/1/AIAA-2006-2212-827.pd
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/77166/1/AIAA-2007-2272-508.pd
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/76198/1/AIAA-2006-7951-158.pd
Thermomechanical analysis of the space shuttle tile thermal protection system (TPS) subjected to dam...
Research on the effects of damage on the thermomechanical performance and structural integrity of th...
At the end of Space Shuttle mission, it re-enters the earth\u27s atmosphere with a speed that exceed...
Thermal protection materials and systems (TPS) are used to protect space vehicles from the heat expe...
The reusable surface insulation (RSI) material used in the shuttle thermal protection system is susc...
The characteristics and development of a lightweight reusable thermal protection system for the spac...
The TPS (Thermal Protection System) is a subsystem providing protection and isolation from aerodynam...
Thermal protection systems for hypersonic vehicles are low- to zero-fault-tolerant. In order to unde...
Spacecraft entering a planetary atmosphere require a very sophisticated thermal protection system. T...
The objective of this work has been to develop more efficient, lighter weight, and higher temperatur...
The major material and design challenges associated with the orbiter thermal protection system (TPS)...
During its lifetime a space launcher is subjected to extreme heat loads. These can dramatically infl...
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