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Development of the Multi-Purpose Transportation System for the Space Launch System (SLS) Core Stage (CS) Flight ArticleNASA's Multi-Purpose Transportation System (MPTS) is designed to transport the Space Launch System (SLS) vehicle segments by waterway and roadway. It is tasked with transporting the vehicle from where it is manufactured to its intermediate test location and final launch destination. Its design incorporates mechanisms that release degrees of freedom to prevent excessive loading during transit and ensure a successful delivery of the vehicle to its intended destination. In addition to the Core Stage (CS) flight article, the system will also move three Structural Test Articles (STAs), the Dynamic Demonstration Unit (DDU), and a simulated CS Pathfinder (weight, center of gravity, outer mold line dimensions, and overall length) over road terrain at four NASA centers and on the Pegasus barge. The MPTS independently supports the article at both ends while operating as a combined unit through automated monitoring of its released degree of freedom and corrective responses. This allows the system to constrain its payload in a statically determinate manner while traversing highly variable terrain. Multi-body simulation of the transportation route is useful to predict free-body motion within its range of mobility. The MPTS has completed its design and analysis developmental cycles. This paper describes the design challenges encountered in developing this system of large-scale structure, which incorporates complex mechanisms. The unique techniques and methodologies developed for analytical assessment of the hardware are also discussed.
Document ID
20180005157
Acquisition Source
Marshall Space Flight Center
Document Type
Conference Paper
Authors
Sandridge, Sarah
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Lien, Hue
(Jacobs Engineering and Science Services and Skills Augmentation Group (ESSSA) Huntsville, AL, United States)
Hunt, Ronald
(Jacobs Engineering and Science Services and Skills Augmentation Group (ESSSA) Huntsville, AL, United States)
Reese, Ayana
(Jacobs Engineering and Science Services and Skills Augmentation Group (ESSSA) Huntsville, AL, United States)
Doktor, Christopher
(Jacobs Engineering and Science Services and Skills Augmentation Group (ESSSA) Huntsville, AL, United States)
Date Acquired
September 7, 2018
Publication Date
May 16, 2018
Subject Category
Launch Vehicles And Launch Operations
Report/Patent Number
M18-6517
Report Number: M18-6517
Meeting Information
Meeting: Aerospace Mechanisms Symposium
Location: Cleveland, OH
Country: United States
Start Date: May 16, 2018
End Date: May 18, 2018
Sponsors: Mechanisms Education Association
Distribution Limits
Public
Copyright
Public Use Permitted.
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