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European Service Module - Structural Test Article (E-STA) Building Block Test Approach and Model Correlation ObservationsThe Orion European Service Module - Structural Test Article (E-STA) underwent sine vibration testing in 2016 using the Mechanical Vibration Facility (MVF) multi-axis shaker system at NASA Glenn Research Center’s (GRC) Plum Brook Station (PBS) Space Power Facility (SPF). The main objective was to verify the structural integrity of the European Service Module (ESM) under sine sweep dynamic qualification vibration testing. A secondary objective was to perform a fixed-base modal survey, while E-STA was still mounted to MVF, in order to achieve a test correlate the finite element model (FEM). To facilitate the E-STA system level correlation effort, a building block test approach was implemented. Modal tests were performed on two major subassemblies, the crew module/launch abort structure (CM/LAS) and the crew module adapter (CMA) mass simulators. These subassembly FEMs were individually correlated and then integrated into the E-STA FEM prior to the start of the E-STA sine vibration test. This paper summarizes the modal testing and model correlation efforts of both of these subassemblies and how the building block approach assisted in the overall correlation of the E-STA FEM. This paper will also cover modeling practices that should be avoided, recommended instrumentation positioning on complex structures, and the importance of the FEM geometrically matching CAD in sufficient detail in order to adequately replicate internal load paths. The goal of this paper is to inform the reader of the hard earned lessons learned and pitfalls to avoid when applying a building block test approach.
Document ID
20190001819
Acquisition Source
Glenn Research Center
Document Type
Conference Paper
Authors
Winkel, James P.
(NASA Glenn Research Center Cleveland, OH, United States)
Bittinger, Samantha A.
(NASA Glenn Research Center Cleveland, OH, United States)
Suarez, Vicente J.
(NASA Glenn Research Center Cleveland, OH, United States)
Akers, James C.
(NASA Glenn Research Center Cleveland, OH, United States)
Date Acquired
March 22, 2019
Publication Date
January 28, 2019
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
GRC-E-DAA-TN61845
Report Number: GRC-E-DAA-TN61845
Meeting Information
Meeting: International Modal Analysis Conference (IMAC)
Location: Orlando, FL
Country: United States
Start Date: January 28, 2019
End Date: January 31, 2019
Sponsors: Society of Experimental Mechanics, Inc.
Funding Number(s)
WBS: WBS 747797.02.04.30.03
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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