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Design for Safety - The Ares Launch Vehicles Paradigm ChangeThe lessons learned from the S&MA early involvement in the Ares I launch vehicle design phases proved that performing an in-line function jointly with engineering is critical for S&MA to have an effective role in supporting the system, element, and component design. These lessons learned were used to effectively support the Ares V conceptual design phase and planning for post conceptual design phases. The Top level Conceptual LOM assessment for Ares V performed by the S&MA community jointly with the engineering Advanced Concept Office (ACO) was influential in the final selection of the Ares V system configuration. Post conceptual phase, extensive reliability effort should be planned to support future Heavy Lift Launch Vehicles (HLLV) design. In-depth reliability analysis involving the design, manufacturing, and system engineering communities is critical to understand design and process uncertainties and system integrated failures.
Document ID
20100023310
Acquisition Source
Marshall Space Flight Center
Document Type
Presentation
Authors
Safie, Fayssal M.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Maggio, Gaspare
(Information Systems Labs., Inc. Huntsville, AL, United States)
Date Acquired
August 24, 2013
Publication Date
May 19, 2010
Subject Category
Launch Vehicles And Launch Operations
Report/Patent Number
M10-0650
Report Number: M10-0650
Meeting Information
Meeting: 4th IAASS Conference: Making Safety Matter
Location: Huntsville, AL
Country: United States
Start Date: May 19, 2010
End Date: May 21, 2010
Sponsors: International Association for the Advancement of Space Safety
Distribution Limits
Public
Copyright
Public Use Permitted.
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