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DAY: Wednesday |
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05/10/00 |
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Keynote: Missiles and Rockets in Future Military Operations-Technology
Challenges for the Compact Kinetic Energy Missile
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George Snyder |
U.S. Army Aviation & Missile Command |
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Session I: Heatshield Materials and Experimental Performance
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Bill Nourse |
U.S. Army Aviation & Missile Command |
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The Navy Program to Develop Non-Rayon, Carbon-Phenolic, Heatshield Materials-Development History and Overview
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Mark Opeka |
NSWC Carderock |
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Alternate/Low-Cost Materials for Navy Reentry Body Heatshields-Material Properties and Aerothermal Testing
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Stuart Starrett |
Southern Research Institute |
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Evaluation of Carbon-Phenolic Materials for Naval Re-Entry Body and Hypersonic Vehicle Heatshield Applications
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Leslie Cohen |
Fiber Materials, Inc. |
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Ablative Performance of Alternate Carbon-Phenolic Heatshield Composites
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Rex Farmer |
Air Force Research Laboratory |
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Ablation Test Results of a Braided Quartz/Phenolic Heatshield Material
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Paul Martin |
Fiber Materials, Inc. |
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High Performance Non-Toxic Intumescent Coatings
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Samuel Gottfried |
NoFire Technologies |
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Thermal Protection System Development for the Hypersonic Weapons Technology
Program
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Michael Rembert |
Aerotherm Corporation |
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Aerothermal Performance of Candidate Heat Shield Materials for Wedge
Models in a Mach 5 Sled Test Environment
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Gerald Russell |
U.S. Army Aviation & Missile Command |
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Advanced Ceramic Matrix Composites for Hypersonic Applications
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Bob Klacka |
Honeywell Advanced Composites, Inc. |
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Advances in Near Net Shape Forming and Coating of Erosion Resistant Ultra
High Temperature Materials
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Timothy McKechnie |
Plasma Process, Inc. |
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Aerothermal Testing of HyTech Scramjet Inlet Materials
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Ray Dirling, Jr. |
Science Applications International Corporation |
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A Database for High Temperature Material Properties
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Rachael Missri |
Materials Sciences Corporation |
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National Advanced Materials Information System
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Jeff Guthrie |
AMPTIAC |
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Session II: Analysis and Design Tools
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Mark Opeka |
NSWC Carderock |
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Time-Lag Effects of Hyperbollic Conduction on Heat Shield Applications
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S. Han |
Tennessee Technological University |
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Coupled Aerodynamic/Thermal Analysis for Heatshield Designs
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Alvin Murray |
Aerotherm Corporation |
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DAY: Thursday |
DATE: |
05/11/00 |
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Session III: Thermal Protection System Design & Manufacturing
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Rex Farmer |
Air Force Research Laboratory |
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Thermal Protection System Design Requirements for Global Reach
Maneuverable Reentry Systems
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Kei Lau |
The Boeing Company |
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Lightweight Multi-Layer Heatshield Materials for Transatmospheric and
Planetary Entry Vehicles
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H.H. Legner |
Physical Sciences, Inc. |
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Advanced Endo-Atmospheric, Kinetic Kill Vehicle (KKV) Airframe
Weight and Cost Optimization Study for Enhanced Dynamic Performance
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Andrew B. Facciano |
Raytheon Missile Systems Company |
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Advanced Materials Studies for Missile Integrated Heatshield Applications
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K. Wu |
Florida International University |
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Development of a Composite Nosecone for the Next Generation Standard Missile
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John Herold |
Raytheon Missile Systems Company |
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Analysis and Design of a Composite Nosecone for the Next Generation Standard Missile
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Kent Buesking |
Materials Research & Design, Inc. |
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Composite Nosecone for the Next Generation Standard Missile -
Material Properties and Verification Testing
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Samuel Causey |
Southern Research Institute |
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Thermostructural Design of a Hyper-X Leading Edge Aerothermal
Test Specimen
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Ray Dirling, Jr. |
Science Applications International Corporation |
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Acusil Lightweight Thermal Protection System
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J.E. Zimmer |
Aerotherm Corporation |
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Carbon Aerogel Thermal Protection System for Space Operation Vehicles
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Scott Brown |
Southern Research Institute |
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Low Cost Reentry Body Heatshields
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Sheryl Cossins |
Lockheed Martin Space Systems Company |
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New Families of Lightweight Charring Ablators for Diverse Heating
Environments forom 10 to 1000 Btu/FT2 - Sec
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William Congdon |
Applied Research Associates, Inc. |
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Advanced Cnc Manufacturing of Composite Thermal Protection Systems
for Hypersonic Missiles and Entry Vehicles
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William Congdon |
Applied Research Associates, Inc. |
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The Solar Probe Heatshield Development
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J.E. Randolph |
Jet Propulsion Laboratory |
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Session IV: Test Facilities and Capabilities
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Bill Schoenfeld |
Holloman High Speed Test Track |
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Thermal Protection System Rocket Sled Testing
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Mishawn Leadingham |
Holloman High Speed Test Track |
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Thermal Protection on Hypersonic Vehicles
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Craig Schmitz |
AZ Technology |
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Pressure and Temperature Predictions During High Speed Sled-Track Tests
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George Stickford |
Battelle |
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Radiative Calibration of Heat Flux Sensors at NIST: Facilities and
Techniques
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B.K. Tsai |
National Institute of Standards and Technology |
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High Temperature Material Performance Testing Using High Power Continuous
Wave Carbon Dioxide Lasers
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Tim Johnson |
Anteon Corporation |
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EXTRA PAPERS
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High-Temperature Materials for Hypersonic Missiles
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Mark Opeka |
NSWC Carderock |
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New Technology for High-Performance Insulation Materials
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Milton Schick |
Infinite Materials & Products, Inc. |
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