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NASA Marshall Space Flight Center Human Factors Engineering Analysis of Various Hatch Sizes and Associated Safety ImpactsThe NASA Docking System (NDS) is a 31.5-inch (800-millimeter)-diameter circular hatch for astronauts to pass through when docked to other pressurized elements in space or for surface egress. The NDS is utilized on the Orion Spacecraft and has been implemented as the International Docking System Standard (IDSS). The EV74 Human Factors Engineering (HFE) Team at NASA’s Marshall Space Flight Center (MSFC) conducted human factors analyses with various hatch shapes and sizes to accommodate for all astronaut anthropometries, task comfort, and task safety. The 32-inch hatch is too small and a bigger hatch size would better accommodate most astronauts and prove to be safer for daily pass-throughs. To conduct human factors analyses, four participants were gathered based on anthropometry: 1st female, 5th female, 95th male, and 99th male.
Document ID
20190027372
Acquisition Source
Marshall Space Flight Center
Document Type
Conference Paper
Authors
Andrews, Tanya C.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Stewart, Rebecca
(Jacobs Engineering Group Huntsville, AL, United States)
Deitzler, Walter
(Jacobs Engineering Group Huntsville, AL, United States)
Date Acquired
July 17, 2019
Publication Date
May 15, 2019
Subject Category
Spacecraft Design, Testing And Performance
Man/System Technology And Life Support
Report/Patent Number
M19-7340
Meeting Information
Meeting: Annual International Association for the Advancement of Space Safety Conference (IAASS 2019): Space Safety is no Accident
Location: El Segundo, CA
Country: United States
Start Date: May 15, 2019
End Date: May 17, 2019
Sponsors: International Association for the Advancement of Space Safety
Distribution Limits
Public
Copyright
Public Use Permitted.
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