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Global Ecosystem Dynamics Investigation (GEDI) Structural Verification Unit (SVU) Vibration TestThis presentation describes the vibration test campaign of the Structural Verification Unit for the Global Ecosystem Dynamics Investigation (GEDI) mission The Structural Verification Unit test campaign served multiple purposes including the qualification of the instrument primary structure, verification of the structure's stiffness, Aperture Control Mechanism assembly level verification, and validation of the control approach for protoflight instrument vibration testing. Testing included three axes of sine burst, random, and sine vibration excitation. This test sequence required a high number of response instrumentation sensors that included tri-axial accelerometers and tri-axial force gauges. Multiple response limiting methods that included acceleration, force, and moment measurements were used to ensure the safety of the flight hardware. The lessons and specific test details learned on the structural verification unit test campaign will reduce test risks for the upcoming instrument-level vibration tests.
Document ID
20180006158
Acquisition Source
Goddard Space Flight Center
Document Type
Presentation
Authors
Skinner, Chck
(NASA Goddard Space Flight Center Greenbelt, MD, United States)
Date Acquired
October 9, 2018
Publication Date
August 21, 2018
Subject Category
Earth Resources And Remote Sensing
Report/Patent Number
GSFC-E-DAA-TN58975
Meeting Information
Meeting: Structures, Loads, and Dynamics,and Mechanical Systems (SLaMS) Early Career Forum
Location: Greenbelt, MD
Country: United States
Start Date: August 21, 2018
End Date: August 24, 2018
Sponsors: NASA Goddard Space Flight Center
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Keywords
Structural Verification Unit
Aperture Control Mechanism
Global Ecosystem Dynamics Investigation
vibration test
GEDI
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