A flight rated liquid cooled garment system for use inside a full pressure suit has been designed, fabricated, and tested. High temperature tests with this system have indicated that heat is absorbed at a rate decreasing from 224 kg-cal/hr to 143 kg-cal/hr over a 40-min period. The first 30 min are very comfortable; thereafter a gradual heat load builds that results in mild sweating at the end of the 40-min period. In flight tests during hot weather when this cooling system was worn under a regulation flight suit, the pilot reported that temperatures were comfortable and that the garment prevented sweating
Future exploration missions require the development of a new liquid cooling garment (LCG) to support...
Heat stress is a well documented hazard across industries. The combination of environmental conditio...
A Human-In-The-Loop (HITL) Portable Life Support System 2.0 (PLSS 2.0) test has been conducted at NA...
The NASA liquid cooling/ventilating garment (LCVG) currently in use was developed over 40 years ago....
Liquid cooled garments employed in several applications in which severe heat is encountered are disc...
An automatic controller for liquid cooled space suits is reported that utilizes human sweat rate as ...
Future manned space exploration missions will require space suits with capabilities beyond the curre...
Current NASA flight rules limit the maximum cabin temperature (23.9 C) during re-entry and landing t...
Experimental results for three subjects walking on a treadmill at exercise rates of up to 590 watts ...
Discusses use of NREL's thermal comfort tools to test liquid cooling garments for NASA spacesuits
Test data and a mathematical model of the human thermoregulatory system were used to investigate con...
The heat exchange properties of aircrew clothing including a Constant Wear Immersion Suit (CWIS), an...
Future EVA suits need processes and systems to control internal temperature and humidity without ven...
The heat exchange properties of aircrew clothing including a Constant Wear Immersion Suit (CWIS), an...
Automatic temperature control for liquid cooling garments used during astronaut extravehicular activ...
Future exploration missions require the development of a new liquid cooling garment (LCG) to support...
Heat stress is a well documented hazard across industries. The combination of environmental conditio...
A Human-In-The-Loop (HITL) Portable Life Support System 2.0 (PLSS 2.0) test has been conducted at NA...
The NASA liquid cooling/ventilating garment (LCVG) currently in use was developed over 40 years ago....
Liquid cooled garments employed in several applications in which severe heat is encountered are disc...
An automatic controller for liquid cooled space suits is reported that utilizes human sweat rate as ...
Future manned space exploration missions will require space suits with capabilities beyond the curre...
Current NASA flight rules limit the maximum cabin temperature (23.9 C) during re-entry and landing t...
Experimental results for three subjects walking on a treadmill at exercise rates of up to 590 watts ...
Discusses use of NREL's thermal comfort tools to test liquid cooling garments for NASA spacesuits
Test data and a mathematical model of the human thermoregulatory system were used to investigate con...
The heat exchange properties of aircrew clothing including a Constant Wear Immersion Suit (CWIS), an...
Future EVA suits need processes and systems to control internal temperature and humidity without ven...
The heat exchange properties of aircrew clothing including a Constant Wear Immersion Suit (CWIS), an...
Automatic temperature control for liquid cooling garments used during astronaut extravehicular activ...
Future exploration missions require the development of a new liquid cooling garment (LCG) to support...
Heat stress is a well documented hazard across industries. The combination of environmental conditio...
A Human-In-The-Loop (HITL) Portable Life Support System 2.0 (PLSS 2.0) test has been conducted at NA...