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Development and Sizing of the JWST Integrated Science Instrument Module (ISIM) Metering StructureThe JWST Integrated Science Instrument Module (ISIM) includes a large metering structure (approx. 2m x 2m x 1.5m) that houses the science instruments and guider. Stringent dimensional stability and repeatability requirements combined with mass limitations led to the selection of a composite bonded frame design comprised of biased laminate tubes. Even with the superb material specific stiffness, achieving the required frequency for the given mass allocations in conjunction with severe spatial limitations imposed by the instrument complement has proven challenging. In response to the challenge, the ISIM structure team considered literally over 100 primary structure topology and kinematic mount configurations, and settled on a concept comprised of over 70 m of tubes, over 50 bonded joint assemblies, and a "split bi-pod" kinematic mount configuration. In this paper, we review the evolution of the ISIM primary structure topology and kinematic mount configuration to the current baseline concept.
Document ID
20060046733
Acquisition Source
Goddard Space Flight Center
Document Type
Conference Paper
Authors
Johnston, John
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Kunt, Cengiz
(Swales Aerospace Beltsville, MD, United States)
Bartoszyk, Andrew
(Swales Aerospace Beltsville, MD, United States)
Hendricks, Steve
(Swales Aerospace Beltsville, MD, United States)
Cofie, Emmanuel
(Mega United States)
Date Acquired
August 23, 2013
Publication Date
January 1, 2006
Subject Category
Structural Mechanics
Meeting Information
Meeting: SPIE Optomechanical Technologies for Astronomy
Location: Orlando, FL
Country: United States
Start Date: May 24, 2006
End Date: May 31, 2006
Distribution Limits
Public
Copyright
Public Use Permitted.
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