The liquid cooling and ventilation garment (LCGV) is a lifeline for astronauts working in space. Without the use of the LCVG, astronauts would be subject to the extreme temperature swings of the outside environment and inevitably create a hostile environment within the extravehicular mobility unit (EMU). This paper will discuss the physiological and psychological reactions related to extreme body temperature changes. Furthermore, a discussion is provided detailing how different environments influence the thermal efficiency of the LCVG in relation to varying workloads. Two Personal interviews with former astronauts with extravehicular activity (EVA) time, as well as a literature review, will lend insight regarding how the LCVG interacts with...
A flight rated liquid cooled garment system for use inside a full pressure suit has been designed, f...
The concept proposed in this paper is to improve thermal efficiencies of the liquid cooling and vent...
Current NASA flight rules limit the maximum cabin temperature (23.9 C) during re-entry and landing t...
The NASA liquid cooling/ventilating garment (LCVG) currently in use was developed over 40 years ago....
The two flight suits currently worn by crew members during Shuttle launch and landing, the Launch an...
Heat stress is a well documented hazard across industries. The combination of environmental conditio...
For nearly 60 years, astronauts have ventured outside of their spacecraft into the extreme environme...
Extra-vehicular activities (EVA) on Mars will require suits with sophisticated thermal control syste...
Current aircrew protective clothing is unable to the address the challenging situation that arises w...
An improved, temperature control concept is developed, for liquid cooling garments used during astro...
Liquid cooled garments employed in several applications in which severe heat is encountered are disc...
Daily life for firefighters consists of working with life-threatening hazards in hostile environment...
The effects of interior conventional lifeboat temperatures on the thermoregulatory responses of part...
The heat exchange properties of aircrew clothing including a Constant Wear Immersion Suit (CWIS), an...
The heat exchange properties of aircrew clothing including a Constant Wear Immersion Suit (CWIS), an...
A flight rated liquid cooled garment system for use inside a full pressure suit has been designed, f...
The concept proposed in this paper is to improve thermal efficiencies of the liquid cooling and vent...
Current NASA flight rules limit the maximum cabin temperature (23.9 C) during re-entry and landing t...
The NASA liquid cooling/ventilating garment (LCVG) currently in use was developed over 40 years ago....
The two flight suits currently worn by crew members during Shuttle launch and landing, the Launch an...
Heat stress is a well documented hazard across industries. The combination of environmental conditio...
For nearly 60 years, astronauts have ventured outside of their spacecraft into the extreme environme...
Extra-vehicular activities (EVA) on Mars will require suits with sophisticated thermal control syste...
Current aircrew protective clothing is unable to the address the challenging situation that arises w...
An improved, temperature control concept is developed, for liquid cooling garments used during astro...
Liquid cooled garments employed in several applications in which severe heat is encountered are disc...
Daily life for firefighters consists of working with life-threatening hazards in hostile environment...
The effects of interior conventional lifeboat temperatures on the thermoregulatory responses of part...
The heat exchange properties of aircrew clothing including a Constant Wear Immersion Suit (CWIS), an...
The heat exchange properties of aircrew clothing including a Constant Wear Immersion Suit (CWIS), an...
A flight rated liquid cooled garment system for use inside a full pressure suit has been designed, f...
The concept proposed in this paper is to improve thermal efficiencies of the liquid cooling and vent...
Current NASA flight rules limit the maximum cabin temperature (23.9 C) during re-entry and landing t...