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EVA Design, Verification, and On-Orbit Operations Support Using Worksite AnalysisThe International Space Station (ISS) design is a very large and complex orbiting structure with thousands of Extravehicular Activity (EVA) worksites. These worksites are used to assemble and maintain the ISS. The challenge facing EVA designers was how to design, verify, and operationally support such a large number of worksites within cost and schedule. This has been solved through the practical use of computer aided design (CAD) graphical techniques that have been developed and used with a high degree of success over the past decade. The EVA design process allows analysts to work concurrently with hardware designers so that EVA equipment can be incorporated and structures configured to allow for EVA access and manipulation. Compliance with EVA requirements is strictly enforced during the design process. These techniques and procedures, coupled with neutral buoyancy underwater testing, have proven most valuable in the development, verification, and on-orbit support of planned or contingency EVA worksites.
Document ID
20000067662
Acquisition Source
Marshall Space Flight Center
Document Type
Preprint (Draft being sent to journal)
Authors
Hagale, Thomas J.
(Boeing Co. Huntington Beach, CA United States)
Price, Larry R.
(Boeing Co. Huntington Beach, CA United States)
Date Acquired
September 7, 2013
Publication Date
January 1, 2000
Publication Information
ISSN: 0148-7191
Subject Category
Man/System Technology And Life Support
Report/Patent Number
SAE-TPS-00ICES-208
ISSN: 0148-7191
Report Number: SAE-TPS-00ICES-208
Meeting Information
Meeting: 30th International Conference on Environmental Systems
Location: Toulouse
Country: France
Start Date: July 10, 2000
End Date: July 13, 2000
Sponsors: Engineering Society for Advancing Mobility Land, Sea
Funding Number(s)
CONTRACT_GRANT: NAS8-39400
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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