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Reconstruction of Ares I-X Integrated Vehicle Rollout LoadsThe measurements taken during the Ares I-X test flight provided a unique opportunity to assess the accuracy of the models and methods used to analyze the loads and accelerations present in the planned Ares I vehicle. During the rollout of the integrated vehicle from the Vehicle Assembly Building (VAB) to the launch pad, the vehicle and its supporting structure are subjected to wind loads and the vibrations produced by the crawler-transporter (CT) that is carrying it. While the loads induced on the vehicle during this period are generally low relative to those experienced in flight, the rollout is a period of operation of primary interest to those designing both the ground support equipment and the interfaces between the launch vehicle and its supporting structure. In this paper, the methods used for reconstructing the loads during the rollout phase are described. The results generated are compared to measured values, leading to insight into the accuracy of the Ares I assessment techniques.
Document ID
20110014752
Acquisition Source
Marshall Space Flight Center
Document Type
Conference Paper
Authors
Chamberlain, Matthew K.
(Dynamic Concepts, Inc. Huntsville, AL, United States)
Hahn, Steven R.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
August 25, 2013
Publication Date
April 4, 2011
Subject Category
Ground Support Systems And Facilities (Space)
Report/Patent Number
M11-0345
Meeting Information
Meeting: 52nd AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference
Location: Denver, CO
Country: United States
Start Date: April 4, 2011
End Date: April 7, 2011
Sponsors: American Helicopter Society, Inc., American Inst. of Aeronautics and Astronautics, American Society of Civil Engineers, American Society of Mechanical Engineers
Funding Number(s)
TASK: NNM08AB71T
Distribution Limits
Public
Copyright
Public Use Permitted.
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