Reflections on Centaur Upper Stage Integration by the NASA Lewis (Glenn) Research Center
Author(s) -
Scott Graham
Publication year - 2014
Publication title -
49th aiaa/asme/sae/asee joint propulsion conference
Language(s) - English
Resource type - Conference proceedings
DOI - 10.2514/6.2014-3670
Subject(s) - centaur , center (category theory) , computer science , stage (stratigraphy) , aeronautics , aerospace engineering , astrobiology , engineering , geology , physics , astronomy , paleontology , chemistry , crystallography
The NASA Glenn (then Lewis) Research Center (GRC) led several expendable launch vehicle (ELV) projects from 1963 to 1998, most notably the Centaur upper stage. These major, comprehensive projects included system management, system development, integration (both payload and stage), and launch operations. The integration role that GRC pioneered was truly unique and highly successful. Its philosophy, scope, and content were not just invaluable to the missions and vehicles it supported, but also had significant Agency-wide benefits. An overview of the NASA Lewis Research Center (now the NASA Glenn Research Center) philosophy on ELV integration is provided, focusing on Atlas/Centaur, Titan/Centaur, and Shuttle/Centaur vehicles and programs. The necessity of having a stable, highly technically competent in-house staff is discussed. Significant depth of technical penetration of contractor work is another critical component. Functioning as a cohesive team was more than a concept: GRC senior management, NASA Headquarters, contractors, payload users, and all staff worked together. The scope, content, and history of launch vehicle integration at GRC are broadly discussed. Payload integration is compared to stage development integration in terms of engineering and organization. Finally, the transition from buying launch vehicles to buying launch services is discussed, and thoughts on future possibilities of employing the successful GRC experience in integrating ELV systems like Centaur are explored.
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