2004 Proceedings

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. However, some of these presentations are available in PowerPoint format and denoted by an asterisk (*). To obtain a copy of these presentations, contact sclv-workshop@aero.org. All documents are posted with permission.

Tuesday, June 22, 2004

Morning (8:30 a.m.)

1. Mission Success Col Dewan, Space and Missle Systems Center
2. Dynamic and Impact Analysis of Aerospace Vehicles using ABAQUS/Explicit
   K. Indermuehle, ATA Engineering, Inc.
3. Impact of Component Parameter Uncertainties on Coupled Loads Analysis Results A. Majed and E. Henkel, Applied Structural Dynamics, Inc.
4. Improved Mixed-Boundary Component-Mode Representation for Structural Dynamic Analysis A. Majed and E. Henkel, Applied Structural Dynamics, Inc.
5. Identification of Overpressure Sources at Launch Vehicle Lift-off Using an Inverse Method B. Troclet, EADS ST
6. Rocket Engine Nozzle Side Load Transient Analysis J. Shi and J. Beck, The Boeing Company
   

Tuesday, June 22, 2004

Afternoon (12:30 p.m.)

1. Qualifying Spirit and Opportunity to Martian Landing Loads with Centrifuge Testing G. Davis and M. Coleman, Jet Propulsion Laboratory
2. On the Semi-Empirical Method for Force Limited Vibration Y. Soucy, Canadian Space Agency, and V. Dharanipathi & R. Sedaghati, Concordia University
3. Measuring Random Vibrations S. Welaratna, Data Physics Corporation
4. V-Band Separation Test Results K. Chang, Jet Propulsion Laboratory
5. Relational Database Design for the Vibroacoustic Intelligent System for Predicting Environments, Risk, and Specifications (VISPERS) Software Suite M. Boeck, B. W. Wong, and B. K. Wong, The Aerospace Corporation

Wednesday, June 23, 2004

Morning (8:30 a.m.)

1. The Standard Deviation of Launch Vehicle Environments C. Krueger, Analex Corp/KSC and I. Yunis, NASA Kennedy Space Flight Center
2. A Comparison of Base-Shake and Mode-Survey Test Based Model Correlation Techniques J. Lollock, The Aerospace Corporation
3. Modeling of Ball Bearing Induced Vibration M. Lee and A. Leveille, The Aerospace Corporation
4. Jitter Analysis of a Large Spacecraft S. Mittal, Lockheed Martin Space Systems Company
5. Mid-Frequency Band Nonlinear Structural Dynamics of Large Space Structures D. Adams, Jet Propulsion Laboratory, and B. Coppolino, Measurement Analysis Corp.
6. Vibro-Acoustic Analysis of Complex Systems: The Hybrid FE-SEA Approach* P. J. Shorter, ESI US R&D, and R. Langley, Department of Energy, University of Cambridge

Wednesday, June 23, 2004

Afternoon (12:30 p.m.)

1. Panel Session: Modeling and Validation in the Mid-Frequency Range
2. Ensuring Conservatism of the Equivalent Test in the Damage Potential Method  D. Huntington, The Boeing Company
3. Protecting Satellites from the Dynamics of the Launch Environment C. Johnson and P. Wilke, CSA Engineering
4. Attenuation of Transient Vibrations Using a Unique Tuned Vibration Absorber A. Kolaini, J. Jensen, S. Rubin, D. Wong, Z. Duron, and B. Sako, The Aerospace Corporation
5. Araine 5 Lower Engine Frame and Lift-off Case O. Bugnet, CNES
6. Testing, Modeling, and Simulating the Control Surfaces of the X37 Vehicle* M. Bacaloni, The Boeing Company

Thursday, June 24, 2004

Morning (8:30 a.m.)

1. Acoustic Induced Vibration on Structure Mounted on Honeycomb Panel: Test versus Prediction W. B. Tsoi and M. O'Connell, Jet Propulsion Laboratory
2. SEA Vibro-Acoustic Analysis of THEMIS Probe Panels T. Scharton, Consultant
3. Variance of Energy & Confidence Intervals in SEA: Numerical and Experimental Validation* V. Cotoni, ESI US R&D, and R. Langley, Department of Energy, University of Cambridge
4. Vibro-acoustic Analysis of Launch Vehicle Lift-Off Environments with RAYON H. Defosse & M. Hamdi, ESI/STRACO, and B. Gardner, ESI US R&D
5. Computational Structural Acoustics of Aerospace Structures S. Conlon, S. Hambric, J. Fahnine and E. Paterson, Applied Research Laboratory, The Pennsylvania State University
6. Direct Field Acoustic Test and Simulation Analysis F. Hausle, S. Johnston, and J. Stadille, Ball Aerospace and Technologies Corp.