NASA NTRS · 19720023204
Design, develop, fabricate, assemble and checkout and advanced active damper system
Abstract
An active electromagnetic damper system was developed for and used in a 5.5% aeroelastic model of Saturn 1B/SA206 launch configuration in wind tunnel tests to determine ground wind-induced loads. Detailed descriptions are given of the damper development program: approach, design analyses, fabrication, checkout, system calibration, wind tunnel test results, damper assembly and operating instructions, and trouble-shooting procedures. Conclusions and recommendations to improve the damper system for future applications are also presented.
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Chang, C. S.. 1972-03-31. Design, develop, fabricate, assemble and checkout and advanced active damper system. https://ntrs.nasa.gov/citations/19720023204
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