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Title
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Retrofitted Damping Treatment for a Three Stage Booster System
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Description
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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
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Creator
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Segalman, Daniel J.
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Marek, E. L.
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Publisher
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Wright-Patterson Air Force Base, OH : Wright Laboratory, Flight Dynamics Directorate, Air Force Systems Command
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Date
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1991
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Format
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1 online resources (1 page)
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Type
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article
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Abstract
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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
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Date Issued
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1991-08
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Extent
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1
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Corporate Author
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Sandia National Laboratories
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Laboratory
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Wright Laboratory
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Report Number
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WL-TR-91-3078 Volume II, page EDB-1
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DoD Project
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2401
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DoD Task
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240104
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Distribution Conflict
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No
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Index Abstract
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Contrails only
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Photo Quality
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Not Needed
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Distribution Classification
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1
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Report Availability
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Full text available
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Provenance
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University of Colorado Colorado Springs, Kraemer Family Library
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Identifier
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ADA241312
