Ergonomics design and test for China “Feitian” EVA spacesuit
- Paper number
IAC-10.A1.6.10
- Author
Mr. Li Tanqiu, China Astronaut Research and Training Center, China
- Year
2010
- Abstract
China “Feitian” EVA spacesuit is an semi-rigid architecture system which designed for Orbit station service (microgravity environment), its ergonomics capability is one of key performance for EVA mission, this paper describes mobility, visibility ,workspace and operation interface design for the spacesuit and relevant test issue briefly, which includes the configuration of soft joints and airtight bearings, the layout design of workspace and control panel, the structure characters of soft joints and size adjustment according the requirements of EVA task and spacesuit self control . and the methods and results of ergonomics test are also presented.
- Abstract document
- Manuscript document
IAC-10.A1.6.10.pdf (🔒 authorized access only).
To get the manuscript, please contact IAF Secretariat.