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Comparative Ergonomic Evaluation of Spacesuit and Space Vehicle DesignWith the advent of the latest human spaceflight objectives, a series of prototype architectures for a new launch and reentry spacesuit that would be suited to the new mission goals. Four prototype suits were evaluated to compare their performance and enable the selection of the preferred suit components and designs. A consolidated approach to testing was taken: concurrently collecting suit mobility data, seat-suit-vehicle interface clearances, and qualitative assessments of suit performance within the volume of a Multi-Purpose Crew Vehicle mockup. It was necessary to maintain high fidelity in a mockup and use advanced motion-capture technologies in order to achieve the objectives of the study. These seemingly mutually exclusive goals were accommodated with the construction of an optically transparent and fully adjustable frame mockup. The construction of the mockup was such that it could be dimensionally validated rapidly with the motioncapture system. This paper describes the method used to create a space vehicle mockup compatible with use of an optical motion-capture system, the consolidated approach for evaluating spacesuits in action, and a way to use the complex data set resulting from a limited number of test subjects to generate hardware requirements for an entire population. Kinematics, hardware clearance, anthropometry (suited and unsuited), and subjective feedback data were recorded on 15 unsuited and 5 suited subjects. Unsuited subjects were selected chiefly based on their anthropometry in an attempt to find subjects who fell within predefined criteria for medium male, large male, and small female subjects. The suited subjects were selected as a subset of the unsuited medium male subjects and were tested in both unpressurized and pressurized conditions. The prototype spacesuits were each fabricated in a single size to accommodate an approximately average-sized male, so select findings from the suit testing were systematically extrapolated to the extremes of the population to anticipate likely problem areas. This extrapolation was achieved by first comparing suited subjects performance with their unsuited performance, and then applying the results to the entire range of the population. The use of a transparent space vehicle mockup enabled the collection of large amounts of data during human-in-the-loop testing. Mobility data revealed that most of the tested spacesuits had sufficient ranges of motion for the selected tasks to be performed successfully. A suited subject's inability to perform a task most often stemmed from a combination of poor field of view in a seated position, poor dexterity of the pressurized gloves, or from suit/vehicle interface issues. Seat ingress and egress testing showed that problems with anthropometric accommodation did not exclusively occur with the largest or smallest subjects, but also with specific combinations of measurements that led to narrower seat ingress/egress clearance.
Document ID
20130000751
Acquisition Source
Johnson Space Center
Document Type
Conference Paper
Authors
England, Scott
(MEI Technologies, Inc. Houston, TX, United States)
Cowley, Matthew
(Lockheed Martin Corp. Houston, TX, United States)
Benson, Elizabeth
(MEI Technologies, Inc. Houston, TX, United States)
Harvill, Lauren
(Lockheed Martin Corp. Houston, TX, United States)
Blackledge, Christopher
(MEI Technologies, Inc. Houston, TX, United States)
Perez, Esau
(Lockheed Martin Corp. Houston, TX, United States)
Rajulu, Sudhakar
(NASA Johnson Space Center Houston, TX, United States)
Date Acquired
August 27, 2013
Publication Date
July 21, 2012
Subject Category
Man/System Technology And Life Support
Report/Patent Number
JSC-CN-25791
Meeting Information
Meeting: 4th International Conference on Applied Human Factors and Ergonomics
Location: San Francisco, CA
Country: United States
Start Date: July 21, 2012
End Date: July 25, 2012
Distribution Limits
Public
Copyright
Public Use Permitted.
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