Zobrazeno 1 - 10
of 31
pro vyhledávání: '"Grant C. Bue"'
Publikováno v:
SAE International Journal of Aerospace. 4:130-140
The Space Suit Water Membrane Evaporator (SWME) is the baseline heat rejection technology selected for development for the Constellation lunar suit. The Hollow Fiber (HoFi) SWME is being considered for service in the Constellation Space Suit Element
Publikováno v:
43rd International Conference on Environmental Systems.
The development of the Advanced Extravehicular Mobility Unit (AEMU) Portable Life Support System (PLSS) is currently underway at NASA Johnson Space Center. The AEMU PLSS features two new evaporative cooling systems, the Reduced Volume Prototype Space
Publikováno v:
43rd International Conference on Environmental Systems.
This paper describes the design and development of an innovative thermal and humidity control system for future space suits. The system comprises an evaporation cooling and dehumidification garment (ECDG) and a lithium chloride absorber radiator (LCA
Autor:
Gregory Quinn, David Fogg, John W. Steele, Sean Littibridge, Weibo Chen, Grant C. Bue, Nick Mancini
Publikováno v:
43rd International Conference on Environmental Systems.
Future space exploration missions require advanced thermal control systems (TCS) to dissipate heat from spacecraft, rovers, or habitats operating in environments that can vary from extremely hot to extremely cold. A lightweight, reliable TCS is being
Publikováno v:
43rd International Conference on Environmental Systems.
A Venting Gas Trap (VGT) was designed, built, and tested at NASA Johnson Space Center to eliminate dissolved and free gas from the circulating coolant loop of the Orion Environmental Control Life Support System. The VGT was downselected from two diff
Publikováno v:
43rd International Conference on Environmental Systems.
A dual-bed device to maintain the water quality of the Advanced Spacesuit Water Membrane Evaporation (SWME) water recirculation loop has been designed and is undergoing testing. The SWME is a heat rejection device under development at the NASA Johnso
Publikováno v:
43rd International Conference on Environmental Systems.
Autor:
Marlon Cox, Bruce Conger, Matthew Vogel, Colin Campbell, Janice Makinen, Carly Watts, Grant C. Bue, Aaron Colunga
Publikováno v:
42nd International Conference on Environmental Systems.
The Spacesuit Water Membrane Evaporator (SWME) is a heat-rejection device that is being developed to perform thermal control for advanced spacesuits. Cooling is achieved by circulating water from the liquid cooling garment (LCG) through hollow fibers
Publikováno v:
42nd International Conference on Environmental Systems.
Human thermal modeling has considerable long-term utility to human space flight. Such models provide a tool to predict crew survivability in support of vehicle design and to evaluate crew response in untested space environments. It is to the benefit
Publikováno v:
42nd International Conference on Environmental Systems.
A dual-bed device to maintain the water quality of the Advanced Spacesuit Water Membrane Evaporation (SWME) water recirculation loop has been designed and is undergoing testing. The SWME is a heat rejection device under development at the NASA Johnso