Spacecraft and Launch Vehicle Dynamic Environments Workshop

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A Mixed-Boundary Method in Component-Mode Synthesis A. Majed, Applied Structural Dynamics, and Ed Henkel, The Boeing Company
Overpressure Wave at Lift-Off of the Ariane 5 Launcher: Modelization and Validation H. Lambare & E. Louaas, C.N.E.S. (France)
Delta II MECO: High-Frequency High-Force Event I. Yunis, NASA KSC
Delta II MECO Transient: A Payload Perspective S. Gordon, NASA GSFC
A New Type of Sine Burst Test W. B. Haile, Swales Aerospace, Inc. (with sponsorship from NASA GSFC)

The Use of Sinusoidal Base Shake Testing for Modal Parameter Estimation J. Lollock, The Aerospace Corporation
Efficient and Enhanced Options for Experimental Mode Identification R. Coppolino, Measurement Analysis Corporation
Effective Mass of Fluid in Tank Vibration Testing D. Kern & C-P Kuo, Jet Propulsion Laboratory
Effective High-Frequency Impulse Response Test Techniques S. J. DiMaggio & Z. H. Duron, The Aerospace Corporation
A Modal Identification Method for Highly-Symmetric Turbine Rotors S. J. DiMaggio & Z. H. Duron, The Aerospace Corporation, and G. Davis, The Boeing Company - Rocketdyne
Circuit Board Operating Shapes and Failure Identification Using a Laser Doppler Velocimeter N. Roberts, Sandia National Laboratories
Getting the Most Out of Your Vibration Test Equipment S. Hough, PhD, & S. Welaratna, PhD, Data Physics Corporation

A Spacecraft CLA Response Visualization Tool S. Bayman, Boeing Space and Defense Systems
Analysis Before Design: Including Design Optimization to a Dynamic Environment K. Indermuehle & M. Baker, ATA Engineering, and F. Moehrle & S. Humbert, Pratt and Whitney
Extrapolation of Spacecraft Vibration Test Data T. Scharton & B. Tsoi, Jet Propulsion Laboratory, and R. Coppolino, Measurement Analysis Corporation
Structural Loads Prediction in Force-Limited Vibration Testing K. Chang, Jet Propulsion Laboratory
VISPERS Status Report K. Bradford & Don Wong, The Aerospace Corporation

Databased Predictions of Vibroacoustics Environments using VISPERS J. Manning, Cambridge Collaborative, Inc.
The New Pyrotechnic Ignition Instrument in Separation Shock Test Facility S. Ando, NASDA (Japan)
Reduction of Launch Shock Loads on Satellites Using a Shock Isolation System C. Johnson & P. Wilke, CSA Engineering, Inc.
GALEX Telescope Vibration Response Reduction M. Coleman, Jet Propulsion Laboratory
Spectral Errors from Editing Noise Spikes in Shock and Vibration Data D. Huntington, Boeing Space & Defense Systems
Outlier Detection with Statistical Modeling of Spectral Test Data G. Lobser, Lockheed Martin Astronautics

Advanced Acoustic Blanket Concepts for Payload Fairings B. Gardner, B. Burkewitz, & P. Bremner, Vibro-Acoustic Sciences, Inc., C. Fuller, Virginia Tech., and N. Atalla, Univ. Sherbrooke
Control of Noise Transmission into a Composite Cylinder H. Osman, The Boeing Company, and M. Johnson, Virginia Tech
AutoSEA Comparisons with Booster Acoustic Test Results N. E. Tengler, Lockheed Martin Astronautics
Prediction of High Frequency Vibration Responses of NASA Mars Exploration Rover Spacecraft Due to Acoustic Launch Load Using Statistical Energy Analysis H. Hwang, Jet Propulsion Laboratory
Communications/Navigation Outage Forecasting System (C/NOFS) Statistical Energy Analysis (SEA) Model J. Betts, The Aerospace Corporation
Continuing Enhancements to AutoSEA2 for Spacecraft and Launch Vehicle Applications
M. Loewenstein and C. Kaminsky, Vibro-Acoustic Sciences, Inc.