Add to ORKGImagine entering Earths atmosphere after returning from the outer solar system. A heat shield less t...
In 2012, the entry vehicle for the Mars Science Laboratory (MSL) mission was the largest and heavies...
The objective of this work has been to develop more efficient, lighter weight, and higher temperatur...
Radio frequency transmission characteristics of ablation materials for planetary entry vehicle heat ...
In 2012, NASA's mission of landing the Mars Science Laboratory (MSL) on Mars was successful. MSL was...
High-mass planetary surface access is one of NASAs technical challenges involving entry, descent and...
The Thermal Protection System (TPS) protects (insulates) a body from the severe heating encountered ...
The topics addressed are: (1) Space Exploration Initiative (SEI); (2) Aeroassist Flight Experiment (...
Over the last 5 years, the Heatshield for Extreme Entry Environment Technology (HEEET) project has b...
Spacecraft entering a planetary atmosphere require a very sophisticated thermal protection system. T...
Facilities for simulating entry environment and response of ablative materials to simulated entry en...
New tests and analyses are reported that were carried out to resolve testing uncertainties in the or...
With the gradual increase in robotic rover sophistication and the desire for humans to explore the s...
Thermal protection materials and systems (TPS) have been critical to fulfilling humankinds desire to...
A critical problem in the design of Thermal Protection Systems (TPS) for planetary probes and re-ent...
Imagine entering Earths atmosphere after returning from the outer solar system. A heat shield less t...
In 2012, the entry vehicle for the Mars Science Laboratory (MSL) mission was the largest and heavies...
The objective of this work has been to develop more efficient, lighter weight, and higher temperatur...
Radio frequency transmission characteristics of ablation materials for planetary entry vehicle heat ...
In 2012, NASA's mission of landing the Mars Science Laboratory (MSL) on Mars was successful. MSL was...
High-mass planetary surface access is one of NASAs technical challenges involving entry, descent and...
The Thermal Protection System (TPS) protects (insulates) a body from the severe heating encountered ...
The topics addressed are: (1) Space Exploration Initiative (SEI); (2) Aeroassist Flight Experiment (...
Over the last 5 years, the Heatshield for Extreme Entry Environment Technology (HEEET) project has b...
Spacecraft entering a planetary atmosphere require a very sophisticated thermal protection system. T...
Facilities for simulating entry environment and response of ablative materials to simulated entry en...
New tests and analyses are reported that were carried out to resolve testing uncertainties in the or...
With the gradual increase in robotic rover sophistication and the desire for humans to explore the s...
Thermal protection materials and systems (TPS) have been critical to fulfilling humankinds desire to...
A critical problem in the design of Thermal Protection Systems (TPS) for planetary probes and re-ent...
Imagine entering Earths atmosphere after returning from the outer solar system. A heat shield less t...
In 2012, the entry vehicle for the Mars Science Laboratory (MSL) mission was the largest and heavies...
The objective of this work has been to develop more efficient, lighter weight, and higher temperatur...