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Electronic Repair Concepts for Long-Duration SpaceflightConstraints on the mass and volume that can be allocated for electronics spares and repair equipment on long-duration space missions mean that NASA must look at repair strategies beyond the traditional approach, which has been to replace faulty subsystems in a modular form, termed Orbital Replacement Units or Line Replacement Units. Other possible strategies include component and board-level replacement, modular designs that allow reprogramming of less-critical systems to take the place of more critical failed systems, and a blended approach which uses elements of each of these approaches, along with a limited number of Line Replacement Units. This paper presents some of the constraints and considerations that affect the decision on how to approach electronics repair for long duration space missions, and discusses the benefits and limitations of each of the previously mentioned strategies.
Document ID
20070022359
Acquisition Source
Glenn Research Center
Document Type
Conference Paper
Authors
Easton, John
(National Center for Space Exploration Research on Fluids and Combustion Cleveland, OH, United States)
Pettegrew, Richard D.
(National Center for Space Exploration Research on Fluids and Combustion Cleveland, OH, United States)
Struk, Peter M.
(NASA Glenn Research Center Cleveland, OH, United States)
Date Acquired
August 23, 2013
Publication Date
January 8, 2007
Subject Category
Electronics And Electrical Engineering
Report/Patent Number
AIAA Paper 2007-0545
Report Number: AIAA Paper 2007-0545
Meeting Information
Meeting: 45th AIAA Aerospace Sciences Conference
Location: Reno, NV
Country: United States
Start Date: January 8, 2007
End Date: January 11, 2007
Sponsors: American Inst. of Aeronautics and Astronautics
Funding Number(s)
CONTRACT_GRANT: NCC3-975
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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