NASA's Space Launch System: Systems Engineering Approach for Affordability and Mission Success
Author(s) -
John J. Hutt,
Josh Whitehead,
John Hanson
Publication year - 2017
Publication title -
2018 aiaa space and astronautics forum and exposition
Language(s) - English
Resource type - Conference proceedings
SCImago Journal Rank - 0.103
H-Index - 1
DOI - 10.2514/6.2017-5330
Subject(s) - space (punctuation) , systems engineering , space research , space exploration , space launch , computer science , aerospace engineering , launch vehicle , aeronautics , engineering management , engineering , operating system
NASA is working toward the first launch of the Space Launch System, a new, unmatched capability for deep space exploration with launch readiness planned for 2019. Since program start in 2011, SLS has passed several major formal design milestones, and every major element of the vehicle has produced test and flight hardware. The SLS approach to systems engineering has been key to the program’s success. Key aspects of the SLS SE&I approach include: 1) minimizing the number of requirements, 2) elimination of explicit verification requirements, 3) use of certified models of subsystem capability in lieu of requirements when appropriate and 4) certification of capability beyond minimum required capability.
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