Challenges faced by the Entry Descent and Landing (EDL) community include the lack of a matured forebody heatshield thermal protection system (TPS) capable of meeting the demanding entry environments for the high priority in-situ science missions identified in the decadal survey at Venus, Saturn and the Ice Giants, and the continued sustainment of thermal protection systems/materials. In response to the identified shortfall in TPS technologies capable of extreme entry environments NASA's Space Technology Mission Directorate (STMD) and Science Mission Directorate (SMD) initiated the Heatshield for Extreme Entry Environment Technology (HEEET) project which has matured a 3D-Woven TPS to Technology Readiness Level 6 and which is ready for infus...
In 2012, the entry vehicle for the Mars Science Laboratory (MSL) mission was the largest and heavies...
Phenolic Impregnated Carbon Ablator (PICA) was invented in the mid 1990's and due to its relatively ...
The testing of a thermal protection system (TPS) in multiple arc jets and laser facilities is critic...
The Heat Shield for Extreme Entry Environment Technology (HEEET) project seeks to mature a game chan...
A critical problem in the design of Thermal Protection Systems (TPS) for planetary probes and re-ent...
Over the last 5 years, the Heatshield for Extreme Entry Environment Technology (HEEET) project has b...
The objective of the Heatshield for Extreme Entry Environment Technology (HEEET) projects is to matu...
The objective of the Heatshield for Extreme Entry Environment Technology (HEEET) projects is to matu...
Planetary entry vehicles employ ablative TPS materials to shield the aeroshell from entry aeroheatin...
The Office of Chief Technologist (OCT), NASA has identified the need for research and technology dev...
Thermal protection materials and systems (TPS) have been critical to fulfilling humankind's desire t...
NASA's future missions will be more demanding. They require materials to be mass efficient, robust, ...
Thermal protection materials and systems (TPS) have been critical to fulfilling humankinds desire to...
This presentation was part of the session : Poster SessionsSixth International Planetary Probe Works...
Planetary entry vehicles employ ablative TPS materials to shield the aeroshell from entry aeroheatin...
In 2012, the entry vehicle for the Mars Science Laboratory (MSL) mission was the largest and heavies...
Phenolic Impregnated Carbon Ablator (PICA) was invented in the mid 1990's and due to its relatively ...
The testing of a thermal protection system (TPS) in multiple arc jets and laser facilities is critic...
The Heat Shield for Extreme Entry Environment Technology (HEEET) project seeks to mature a game chan...
A critical problem in the design of Thermal Protection Systems (TPS) for planetary probes and re-ent...
Over the last 5 years, the Heatshield for Extreme Entry Environment Technology (HEEET) project has b...
The objective of the Heatshield for Extreme Entry Environment Technology (HEEET) projects is to matu...
The objective of the Heatshield for Extreme Entry Environment Technology (HEEET) projects is to matu...
Planetary entry vehicles employ ablative TPS materials to shield the aeroshell from entry aeroheatin...
The Office of Chief Technologist (OCT), NASA has identified the need for research and technology dev...
Thermal protection materials and systems (TPS) have been critical to fulfilling humankind's desire t...
NASA's future missions will be more demanding. They require materials to be mass efficient, robust, ...
Thermal protection materials and systems (TPS) have been critical to fulfilling humankinds desire to...
This presentation was part of the session : Poster SessionsSixth International Planetary Probe Works...
Planetary entry vehicles employ ablative TPS materials to shield the aeroshell from entry aeroheatin...
In 2012, the entry vehicle for the Mars Science Laboratory (MSL) mission was the largest and heavies...
Phenolic Impregnated Carbon Ablator (PICA) was invented in the mid 1990's and due to its relatively ...
The testing of a thermal protection system (TPS) in multiple arc jets and laser facilities is critic...