The performance of a material is greatly influenced by its thermal and chemical properties. Analytical pyrolysis, when coupled to a GCMS system, is a powerful technique that can unlock the thermal and chemical properties of almost any substance and provide vital information. At NASA, we depend on precise thermal analysis instrumentation for understanding aerospace travel. Our analytical techniques allow us to test materials in the laboratory prior to an actual field test; whether the field test is miles up in the sky or miles underground, the properties of any involved material must be fully studied and understood in the laboratory
Spectroscopic chemical analysis methods and apparatus are disclosed which employ deep ultraviolet (e...
A program is described which seeks to develop an understanding of the effects of dissolved and trapp...
A flight experiment designed to demonstrate current cryogenic heat pipe technology was defined and e...
The NASA James Webb Space Telescope project identified a need to measure water vapor desorption from...
A study was conducted to determine the ability of an all superfluid helium design to meet the perfor...
The composition of fluid phases in the Earth's mantle are significantly affected by oxygen fugacity...
A program was conducted to evaluate and characterize the carbon dioxide-methane (CO2-CH4) decomposit...
The extent of convective and radiative heating for a Titan aerocapture vehicle is investigated. The ...
The stagnation region of a cylinder in a cross flow was used in experiments conducted with both a si...
The design and performance of pointing and control systems for two space infrared telescope facility...
Laminar models agree closely with the pressure evolution and vapor phase temperature stratification ...
This presentation will examine the development of a thermal control system (TCS) for future space mi...
Pressure and heat transfer tests were conducted simulating flight conditions which the space shuttle...
Engineering and performance of warm gas mass expulsion system for attitude control on long space voy...
Possible storable propellant configurations and program plans are evaluated for the space tug. Alter...
Spectroscopic chemical analysis methods and apparatus are disclosed which employ deep ultraviolet (e...
A program is described which seeks to develop an understanding of the effects of dissolved and trapp...
A flight experiment designed to demonstrate current cryogenic heat pipe technology was defined and e...
The NASA James Webb Space Telescope project identified a need to measure water vapor desorption from...
A study was conducted to determine the ability of an all superfluid helium design to meet the perfor...
The composition of fluid phases in the Earth's mantle are significantly affected by oxygen fugacity...
A program was conducted to evaluate and characterize the carbon dioxide-methane (CO2-CH4) decomposit...
The extent of convective and radiative heating for a Titan aerocapture vehicle is investigated. The ...
The stagnation region of a cylinder in a cross flow was used in experiments conducted with both a si...
The design and performance of pointing and control systems for two space infrared telescope facility...
Laminar models agree closely with the pressure evolution and vapor phase temperature stratification ...
This presentation will examine the development of a thermal control system (TCS) for future space mi...
Pressure and heat transfer tests were conducted simulating flight conditions which the space shuttle...
Engineering and performance of warm gas mass expulsion system for attitude control on long space voy...
Possible storable propellant configurations and program plans are evaluated for the space tug. Alter...
Spectroscopic chemical analysis methods and apparatus are disclosed which employ deep ultraviolet (e...
A program is described which seeks to develop an understanding of the effects of dissolved and trapp...
A flight experiment designed to demonstrate current cryogenic heat pipe technology was defined and e...