2007 Proceedings

Spacecraft and Launch Vehicle
Dynamic Environments Workshop

TUESDAY, JUNE 26, 2007

• Welcome – Aimee Lalime, The Aerospace Corporation
  
• Keynote Address – Curtis Larsen, Johnson Space Center
  
• Predicting Motor Dynamic Strain Due to Road Acceleration During Transport and Shipping Using Neural Networks, Alex Hardt, Orbital Sciences Corporation
  
• Validation Methodology of the Solar Wing Deployment Math Model with the Three Gyro Telemetry Data, Earl Hwang, Boeing Satellite Development Center (SDC)
• Shock & Vibration Mitigation, Odilo Vazquez, Form Fit & Function LLC
  
• MIL-STD-810G Will Better Define Dynamic Tests, Wayne Tustin, Equipment Reliability Institute
  
• Structural Acoustic Characterization of Space Shuttle MPS Flow Liners, Michael Allen and Robert Haberman, BBN Technologies
• Prediction and Correlation of an Orbital Express Spacecraft Random Vibration Responses Due to Acoustic Testing Using Statistical Energy Analysis and Boundary Element Method, Joseph Hackel, Ball Aerospace & Technology Corporation
  
• Comparison of Aerodynamic Noise Data from Two Shuttle Wind Tunnel Tests Performed 31 Years Apart, Harry Himelblau, Consultant
  
• A Passive Sound Canceling Material Using Lightweight Embedded Machines, Paul Lu and Gary Hawkins, The Aerospace Corporation
• A Smart Network Sensor System for Distributed, Synchronous Data Acquisition, Alex Karolys, VIP Sensors, Inc.
  
• Multi-body Dynamic Simulation of MSL Rover Rock Landing on Slopes, Mike S. Lih and Chia-Yen Peng, Jet Propulsion Laboratory
  
• Multi-body Dynamic Analysis of Two Separation Events of the Mars Science Laboratory Rover, Marco Bacaloni, The Aerospace Corporation, & Chia-Yen Peng, Jet Propulsion Laboratory
  
• Very High Damping without Loss of Stiffness Can Reduce Launch Loads, L. Porter Davis, Honeywell International, Inc.

WEDNESDAY, JUNE 27, 2007

• Dynamic Characterization of Structural Interfaces, Luc-Olivier Gonidou, CNES Launchers Directorate
  
• Component Frequency Requirements for Coupled Loads Analysis, John Dickens, Lockheed Martin Company
  
• Software Tool for Computing Maximum Von Mises Stress, Eric Martin and Kurt Knutson, ATA Engineering, Inc., & Long Chen, Jet Propulsion Laboratory
  
• Comparison of Direct Field Acoustic Testing with Reverberant Chamber Testing, Michael O’Connell, Jet Propulsion Laboratory
  
• Development of Standard Practices for Direct Nearfield Acoustic Testing, Mike Van Dyke, The Aerospace Corporation
  
• Investigation of Force Limited Vibration Based on Measurements During Spacecraft Vibration Testing, Yvan Soucy & Steeve Montminy, Space Technologies, Canadian Space Agency
  
• Panel Session: Notching Vibration Tests
         Moderator: Terry Scharton, Consultant
         Panelists: Juan Fernandez, Jet Propulsion Laboratory
                             Dick Foss, Lockheed Martin Company
                             Daniel Kaufman, NASA Goddard Space Flight Center
                             Alan Peterson, The Aerospace Corporation
                             Gene Rosenbaum, The Boeing Company
  
                           Yvan Soucy, Space Technologies, Canadian Space Agency

• Determination of Design and Test Criteria for Structural Analysis of Components in Random Vibration Environments Using Probabilistic Methods, Larry Trilling, Ball Aerospace & Technology Corporation
  
• Acoustic and Random Vibration Test and Analysis of the Heliospheric Imager Instrument or STEREO, Gordon Maahs, The Johns Hopkins University Applied Physics Laboratory
  
• Statistical Analysis of Extreme Peaks in Random Vibration Response Data, Ali Kolaini and Ben Doty, Jet Propulsion Laboratory

THURSDAY, JUNE 28, 2007

• Pseudo Velocity Shock Spectrum Mechanical Shock Analysis Overview, Howard Gaberson, Consultant (Retired Navy)
  
• A Study on the Ability to Analytically Predict Mechanical Failure Due to a Pyrotechnic Shock Environment, Sean Keon, Ensign-Bickford Aerospace & Defense
  
• MSL Pyroshock Development Test Program for Shock Mitigation, Juan Fernandez, Jet Propulsion Laboratory
  
• JPL Tunable Beam Pyroshock Simulation System, Ali Kolaini and Juan Fernandez, Jet Propulsion Laboratory
  
• SEA Analysis of Rocketplane Kistler K-1 Launch Vehicle, Bryce Gardner, ESI Group, & Paul Blelloch, ATA Engineering
  
• Effect of Convection Velocity on the Vibration Response of Launch Vehicle Panels, Paul Blelloch, ATA Engineering