Spacecraft and Launch Vehicle Dynamic Environments Workshop

Missing or inactive links indicate that an electronic version (pdf) is not yet available on this Web site. All documents are posted with permission.

Identification of Overpressure Sources at Launch Vehicle Liftoff Using and Inverse Method J. Boyd, T. Hindle, D. Ruebsamen, Honeywell Defense & Space Electronics Systems
Evolved Launch Vibration Isolation System Demonstration Unit Test Results J. Boyd, T. Hindle, D. Ruebsamen, Honeywell Defense & Space Electronics Systems
Overview of the Vibro-Acoustic Launch Protection Equipment at the Air Force Research Laboratory S. Lane, B. Henderson, C. Gerhart, and R. Richard, Air Force Research Laboratory
Overview of the Development of Dynamic Environments for Atlas V Launch Vehicles G. Gibson, S. Janssen, & L. Bradford, Lockheed Martin Astronautics, and R. Groom, The Aerospace Corporation

Design and Verification of the Mars Exploration Rover Primary Payload D. Lee, Jet Propulsion Laboratory
Mars Exploration Rover Airbag Landing Loads Analysis D. Adams, Jet Propulsion Laboratory
GALEX Instrument: Pegasus Launch Temperature Effects on a Frequency Tuned Damped Structure M. Coleman, Jet Propulsion Laboratory
Exact Solution for Coupled (Non-proportional) Damping Time History Response J. Dickens, Lockheed Martin Space Systems Co., Sunnyvale
PACE Acoustic and Sine Vibration Tests and Supporting Analyses M. O'Connell and W. B. Tsoi, Jet Propulsion Laboratory
VISPERS Status Report K. Bradford, The Aerospace Corporation
Society for Machinery Failure Prevention Technology (MFPT) H. Pusey, MFPT Society
Shock & Vibration Information Analysis Center (SAVIAC) J. Leifer, SAVIAC

Random Vibrations and Finite Elements for Modeling Spacecraft and Launch Vehicles Dynamic Environment J. P. Coyette, G. Lielens, P. Ploumhans & JD. Thiebaut, Free Field Technologies
Using Test to Drive Design T. Scharton, C-Y. Peng & W. B. Tsoi, Jet Propulsion Laboratory, and M. Baker, D. Hensley, K. Knutson, & R. Brillhart, ATA Engineering, Inc.
Integrating Structural Analysis and Test at NASA GSFC D. Kaufman, NASA Goddard Space Flight Center
Random Vibration Test of Mars Exploration Rover Spacecraft T. Scharton and D. Lee, Jet Propulsion Laboratory
Reduction of SPOT 5 Mechanical Test Program Based on CLA Information and on Real Time Modal Identification During the Sine Vibrations J-N. Bricout, A. Rolfo, CNES France

Panel Session: Spacecraft Vibration Testing
International Space Station Docking Mechanism: Testing, Modeling, and Dynamic Simulation S. Ghofranian and R. Mar, Boeing Space and Defense Systems
Enigma Multibody Loads Analysis: An Overview K. Parin, E. Henkel, and A. Majed, Applied Structural Dynamics
Analysis of Nonstationary Vibroacoustic Flight Data Using a Damage-Potential Basis S. DiMaggio & B. Sako, The Aerospace Corporation, and S. Rubin, Rubin Engineering Company
Evaluating Fatigue Equivalence Using Measured Vibration Data S. DiMaggio & B. Sako, The Aerospace Corporation, and S. Rubin, Rubin Engineering Company

Reverberant Acoustic Test of Mars Exploration Rover Spacecraft H-J. Wang, Jet Propulsion Laboratory
Modeling Viscoelastic Laminate Sections in Statistical Energy Analysis P. Shorter and B. Gardner, Vibro-Acoustic Sciences/ESI Group
Enhancing Low Frequency Transmission Loss with Heterogeneous Acoustic Blankets B. Gardner, Vibro-Acoustic Sciences/ESI Group and M. R. F. Kidder, Virginia Tech
A New Application of AutoSEA2 for Structural Dynamics Analysis M. E. Wang, V. Rolle, and D. Krebs, The Boeing Company
Correction Level for Salvaging Pyrotechnic Data Using Wavelets L. Smith, Retired
Mars Exploration Rover Brush Motors Pyroshock Test Experience K. Chang, Jet Propulsion Laboratory
A Comment Session on the KSC Shock Failure Prediction Test Program I. Yunis and C. Burke, NASA Kennedy Space Center