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Concurrent engineering: Spacecraft and mission operations system designDespite our awareness of the mission design process, spacecraft historically have been designed and developed by one team and then turned over as a system to the Mission Operations organization to operate on-orbit. By applying concurrent engineering techniques and envisioning operability as an essential characteristic of spacecraft design, tradeoffs can be made in the overall mission design to minimize mission lifetime cost. Lessons learned from previous spacecraft missions will be described, as well as the implementation of concurrent mission operations and spacecraft engineering for the Near Earth Asteroid Rendezvous (NEAR) program.
Document ID
19950011199
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Landshof, J. A.
(Johns Hopkins Univ. Laurel, MD, United States)
Harvey, R. J.
(Johns Hopkins Univ. Laurel, MD, United States)
Marshall, M. H.
(Johns Hopkins Univ. Laurel, MD, United States)
Date Acquired
September 6, 2013
Publication Date
November 1, 1994
Publication Information
Publication: NASA. Goddard Space Flight Center, Third International Symposium on Space Mission Operations and Ground Data Systems, Part 2
Subject Category
Systems Analysis
Accession Number
95N17614
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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