Mass and Consumable Loss Analysis of EVA Spacesuit CCPO System
- Paper number
IAC-13,A1,P,54.p1,x19446
- Author
Mr. Guodong Zhou, China Astronaut Research and Training Center, China
- Coauthor
Mr. Feng Gao, China Astronaut Research and Training Cednter, China
- Coauthor
Mr. Yunze Li, Beihang University, China
- Coauthor
Ms. Shengnan Wang, Beihang University, China
- Coauthor
Mr. Hang Zhou, China
- Year
2013
- Abstract
Mass and consumable loss evaluation models for the extravehicular activity (EVA) spacesuit combined cooling-power-oxygen (CCPO) system were built up. Based on these models, the mass and consumable loss of the CCPO system were calculated at three typical lunar thermal environments, and then compared to other two kinds of cooling, power and oxygen systems. The conclusion indicates that, in reducing consumable loss, the CCPO system has obvious advantage over the other two kinds of systems, and the mass of the CCPO system is acceptable.
- Abstract document
- Manuscript document
(absent)