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Dynamic Stability Finite Element Analysis of Multiple Potential Large Space Telescope Structural DesignsOne of the driving structural requirements of the Habitable Exo-Planet telescope is to maintain line of sight stability between the primary and secondary mirror of ≤ 5 milli-arc seconds. Dynamic analyses of two configurations of a proposed Habitable Exo-Planet 4 meter off-axis telescope structure were performed to predict effects of a vibration input on primary/secondary mirror alignment. The dynamic disturbance used as the forcing function was the James Webb Space Telescope reaction wheel assembly vibration emission specification level. The objective of these analyses was to predict order-of-magnitude performance for various structural configurations which contribute to efforts in defining the Habitable Exo-Planet structural design’s global architecture. Two variations of the basic architectural design were analyzed. Relative motion between the PM and the SM for each design configuration are reported.
Document ID
20230014605
Acquisition Source
Marshall Space Flight Center
Document Type
Presentation
Authors
J. Brent Knight
(Marshall Space Flight Center Redstone Arsenal, Alabama, United States)
H Philip Stahl
(Marshall Space Flight Center Redstone Arsenal, Alabama, United States)
Date Acquired
October 9, 2023
Subject Category
Mechanical Engineering
Meeting Information
Meeting: Alabama Modeling and Simulation Conference
Location: Huntsville, AL
Country: US
Start Date: October 18, 2023
Sponsors: Alabama Modeling and Simulation Conference
Funding Number(s)
WBS: 954879.04.03.62.16
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Technical Review
Single Expert
Keywords
jitter
line of site
dynamic stability
finite element analysis
space telescopes
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