Conferences
2006 Proceedings

Spacecraft and Launch Vehicle
Dynamic Environments Workshop

 

Tuesday, June 27, Morning Session

  1. Prediction of the Dynamic Response of the NASA ACTS Antenna to Wide Spectrum Acoustic Loading Jeffrey Larko, NASA Glenn Research Center; Vincent Cotoni, ESI Group
  2. Derivation of Preliminary Ascent Vibro-Acoustic Environments for the Crew Exploration Vehicle Michael Yang, ATA Engineering, Inc.; Nancy Tengler, Lockheed Martin
  3. Hybrid FE-SEA, Periodic SEA Formulations, and the Energy Flow Method: Combining FE and SEA for New Prediction Tools for Space Structure Vibration and Acoustics Vincent Cotoni and Phil Shorter, ESI Group
  4. Testing of the STEREO Spacecraft Solar Array Subsystem Jennifer R. Tanzman, John Hopkins University Applied Physics Laboratory
  5. FEM-Based Methods for Vibro-Acoustic Response of Non-Uniform Sandwich Panels Paul Blelloch, ATA Engineering, Inc.

Tuesday, June 27, Afternoon Session

  1. Extreme Response Peaks in Random Vibration Tests Terry Scharton, North Carolina State University; David Pankow and Michael Sholl, University of California at Berkeley
  2. Telemetry and Measurements System to Improve the Knowledge of ARIANE 5 Flights Environments, Patrick Mourey and Eric Louaas, CNES Launcher Directorate
  3. Wireless Sensing and Control Systems for Use on Launch Vehicles and Spacecraft Kevin Champaigne, Invocon, Inc.
  4. Piecewise Reconstruction of Single Source Telemetry from Successive Receivers Jorge Seidel, Frank Meng, and Jon King, The Aerospace Corporation
  5. Shock Time History Reconstruction Via Wavelets Tom Irvine, Vibrationdata Corporation
  6. Pyrotechnic Shock Testing: Real Test Lab Experiences at EBA&D Sean Keon, Ensign-Bickford Aerospace and Defense Company

Wednesday, June 28, Morning Session

  1. Use of Stochastic Analysis to Optimize S/C design and to Bring Robustness on the Margins, Jean-Noel Bricout, Emmanuelle Riviere & Stephane Mary, CNES
  2. Team Corporation: Inertial Mass Guided Head Expander Curt Nelson, Team Corporation
  3. Maximum Von Mises Stress in the Loading Environment of Mass Acceleration Curve Robert J. Glaser and Long Y. Chen, Jet Propulsion Laboratory
  4. SoftRide Vibration and Shock Isolation Systems that Protect Spacecraft from Launch Dynamic Environments Conor D. Johnson, Paul S. Wilke, and Scott Pendleton, CSA Engineering, Inc.
  5. Role of Structural Analysis for SpaceShipOne and the Ansari X-Prize Chris Flanigan, Quartus Engineering, Inc.
  6. Integrated Modeling Applied to the Terrestrial Planet Finder Mission Andrew Kissila, Eug Kwacka, Timothy Hoa, Philip Dumonta, Sandra Irishb, Ichung Wengc, aJet Propulsion Laboratory, bGoddard Space Flight Center, cSwales Aerospace

Wednesday, June 28, Afternoon Session

  1. Ground Landing Dynamics of the Crew Exploration Vehicle George Antoun, ATA Engineering, Inc., and Nancy Tengler, Lockheed Martin
  2. A “Super Bowl” Approach to Mars Rover Touchdown Loads Analysis Chia-Yen Peng and Gary Ortiz, Jet Propulsion Laboratory
  3. Review of Changes and Additions within IEST-RP-DTE0112.2: Handbook for Dynamic Data Acquisition and Analysis – 2006 Allan Piersol, Piersol Engineering, Inc., & Harry Himelblau, Independent Consultant
  4. What’s Wrong with Dynamics Test Measurements Today? Charles Wright, The Aerospace Corporation
  5. Two New Breakthroughs In Vibroacoustic Analysis – 160 dB Input Range and a Flat Microphone Mark Serridge, Bruel & Kjaer (North America) Inc., and Flemming Schultz Larsen, Bruel & Kjaer Sound & Vibration (Denmark)
  6. Multiaxis Random Vibration Testing Prior to Launch of Spacecraft and Other Vehicle Wayne Tustin, Equipment Reliability Institute

Thursday, June 29, Morning Session

  1. Required Correlation Standards for Expendable Launch Vehicle Loads Isam Yunis, Tim Fogarty, NASA Kennedy Space Center
  2. Experiences Using an Automated Shaker Selection Algorithm Kevin Napolitano, ATA Engineering
  3. Aliasing in Modal Parameter Estimation Havard Vold, Kevin Napolitano Dan Hensley, ATA and Engineering, Inc.
  4. Reentry Breakup Analysis for Applications in Aerospace Nuclear Safety Lisa Ling, Jet Propulsion Laboratory
  5. Need for Standardization in Pyrotechnic Shock Testing Methods Moderator: Alan Peterson, The Aerospace Corporation


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