Thermal protection materials and systems (TPS) are required to protect a vehicle returning from space or entering an atmosphere. The selection of the material depends on the heat flux, heat load, pressure, and shear and other mechanical loads imposed on the material, which are in turn determined by the vehicle configuration and size, location on the vehicle, speed, a trajectory, and the atmosphere. In all cases the goal is to use a material that is both reliable and efficient for the application. Reliable materials are well understood and have sufficient test data under the appropriate conditions to provide confidence in their performance. Efficiency relates to the behavior of a material under the specific conditions that it encounters TPS ...
The topics addressed are: (1) Space Exploration Initiative (SEI); (2) Aeroassist Flight Experiment (...
This talk outlines work in coatings for TPS done at NASA Ames. coatings and surface treatments on re...
Planetary entry vehicles employ ablative TPS materials to shield the aeroshell from entry aeroheatin...
Thermal protection materials and systems (TPS) protect vehicles from the heat generated when enterin...
Thermal protection materials and systems (TPS) are used to protect space vehicles from the heat expe...
Thermal protection materials and systems (TPS) have been critical to fulfilling humankinds desire to...
High temperature testing of thermal protection system (TPS) materials is a critical aspect of heat-s...
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...
Thermal Protection System Materials & thermal control coatings were characterized by a variety of me...
Planetary entry vehicles employ ablative TPS materials to shield the aeroshell from entry aeroheatin...
During all phases of a spacecraft's mission, a Thermal Protection System (TPS) is needed to protect ...
Since the first U.S. manned entry, Mercury (May 5, 1961), seventy-five manned entries have been made...
High temperature insulation materials for use under radiative thermal protection systems of shuttle ...
A primary focus of the Entry Systems and Technology Division at NASA Ames is design, development, qu...
The topics addressed are: (1) Space Exploration Initiative (SEI); (2) Aeroassist Flight Experiment (...
This talk outlines work in coatings for TPS done at NASA Ames. coatings and surface treatments on re...
Planetary entry vehicles employ ablative TPS materials to shield the aeroshell from entry aeroheatin...
Thermal protection materials and systems (TPS) protect vehicles from the heat generated when enterin...
Thermal protection materials and systems (TPS) are used to protect space vehicles from the heat expe...
Thermal protection materials and systems (TPS) have been critical to fulfilling humankinds desire to...
High temperature testing of thermal protection system (TPS) materials is a critical aspect of heat-s...
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...
Thermal Protection System Materials & thermal control coatings were characterized by a variety of me...
Planetary entry vehicles employ ablative TPS materials to shield the aeroshell from entry aeroheatin...
During all phases of a spacecraft's mission, a Thermal Protection System (TPS) is needed to protect ...
Since the first U.S. manned entry, Mercury (May 5, 1961), seventy-five manned entries have been made...
High temperature insulation materials for use under radiative thermal protection systems of shuttle ...
A primary focus of the Entry Systems and Technology Division at NASA Ames is design, development, qu...
The topics addressed are: (1) Space Exploration Initiative (SEI); (2) Aeroassist Flight Experiment (...
This talk outlines work in coatings for TPS done at NASA Ames. coatings and surface treatments on re...
Planetary entry vehicles employ ablative TPS materials to shield the aeroshell from entry aeroheatin...