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Integrated Modal Test of the Artmis I Launch VehicleThe dynamic testing campaign for the Artemis I launch vehicle culminated in the Integrated Modal Test (IMT). The IMT consisted of the Space Launch System with a mass simulator of Orion (MSO) on top of the SLS stack, which rested on the deck of the mobile launcher (ML) and mount mechanisms. The modal testing met the goal to capture a set of target modes under 7Hz, in two test configurations, using 298 accelerometer locations and 472 accelerometer channels. Overall the model of the test matched very well with the data without tuning the model with the exception of the first torsion mode, which was measured at a much lower frequency than predicted at when excited at higher levels.
Document ID
20230008833
Acquisition Source
Marshall Space Flight Center
Document Type
Presentation
Authors
Dan Lazor
(Marshall Space Flight Center Redstone Arsenal, Alabama, United States)
Clay Fulcher
(Jacobs (United States) Dallas, Texas, United States)
Patrick Hull
(Marshall Space Flight Center Redstone Arsenal, Alabama, United States)
Eric Stewart
(Marshall Space Flight Center Redstone Arsenal, Alabama, United States)
Date Acquired
June 9, 2023
Subject Category
Spacecraft Design, Testing and Performance
Meeting Information
Meeting: Spacecraft and Launch Vehicles Dynamic Environment Workshop
Location: El Segundo, CA
Country: US
Start Date: June 27, 2023
End Date: June 29, 2023
Sponsors: The Aerospace Corporation
Funding Number(s)
WBS: 585777.02.44.06.05.10
Distribution Limits
Public
Copyright
Public Use Permitted.
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