Add to ORKGStudy of extreme temperature requirements for spacecraft electronic piece-parts to be used as thermal design criteria for parts developmen
Heat balances of combined astrionic equipment and thermal conditioning subsystem of environmental co...
The effects of extreme values of surface and low altitude atmospheric parameters on space vehicle de...
Mission planning documents were used to analyze the radiator design and thermal control surface requ...
Extreme temperature determinations which affect spacecraft electronic equipment on flyby mission
Determining temperature extremes in electronic components of spacecraft on interplanetary orbiter an...
Electronic systems capable of extreme temperature operation are required for many future NASA space ...
Guidance for the assessment and control of spacecraft temperatures is provided with emphasis on unma...
Data sheets provide temperature requirements for 82 individual instruments that are under developmen...
Component qualification and acceptance temperatures are derived from worst case thermal analyses and...
The Thermal Control Working Group limited its evaluation to issues associated with Earth orbiting an...
Needs and requirements for a free flying space science and applications platform to host groupings o...
The U.S. space program goals for long-duration manned missions place particular demands on thermal-c...
In the 21st century, the National Aeronautics and Space Administration (NASA), the Russian Federal S...
Considerations associated with design of thermal subsystem of Orbiting Astronomical Observator
The descent module (DM) of the ISS Soyuz vehicle is covered by thermal protection system (TPS) mater...
Heat balances of combined astrionic equipment and thermal conditioning subsystem of environmental co...
The effects of extreme values of surface and low altitude atmospheric parameters on space vehicle de...
Mission planning documents were used to analyze the radiator design and thermal control surface requ...
Extreme temperature determinations which affect spacecraft electronic equipment on flyby mission
Determining temperature extremes in electronic components of spacecraft on interplanetary orbiter an...
Electronic systems capable of extreme temperature operation are required for many future NASA space ...
Guidance for the assessment and control of spacecraft temperatures is provided with emphasis on unma...
Data sheets provide temperature requirements for 82 individual instruments that are under developmen...
Component qualification and acceptance temperatures are derived from worst case thermal analyses and...
The Thermal Control Working Group limited its evaluation to issues associated with Earth orbiting an...
Needs and requirements for a free flying space science and applications platform to host groupings o...
The U.S. space program goals for long-duration manned missions place particular demands on thermal-c...
In the 21st century, the National Aeronautics and Space Administration (NASA), the Russian Federal S...
Considerations associated with design of thermal subsystem of Orbiting Astronomical Observator
The descent module (DM) of the ISS Soyuz vehicle is covered by thermal protection system (TPS) mater...
Heat balances of combined astrionic equipment and thermal conditioning subsystem of environmental co...
The effects of extreme values of surface and low altitude atmospheric parameters on space vehicle de...
Mission planning documents were used to analyze the radiator design and thermal control surface requ...