Retrofitted Damping Treatment for a Three Stage Booster System

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Report Number: WL-TR-91-3078 Volume II, page EDB-1
Author(s): Segalman, Daniel J., Marek, E. L.
Corporate Author(s): Sandia National Laboratories
Laboratory: Wright Laboratory
Date of Publication: 1991-08
Pages: 1
DoD Project: 2401
DoD Task: 240104
Identifier: This paper is part of a conference proceedings. See ADA241312

Abstract:
A three-stage solid propellant booster system has been developed to launch a variety of payloads. A critical issue to the success of any flight is the possible interaction of the elastic vibrational modes with the control system. Modal test results indicate that damping factors may be very low (0

Provenance: University of Colorado Colorado Springs, Kraemer Family Library

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