2013 National Space & Missile Materials Symposium

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Hypersonics continued 1300 - 1325 LCWHS Missile Structures, Dr. Bill Garver, Lockheed Martin 1325 - 1350 Hypersonic Control Surfaces Using the High Density - Low Density Family of Integrated Dual Layer Materials, Mr. James Crowley, Textron Systems Corporation 1350 - 1415 High Temperature Structural Honeycombs, Hat Stiffeners and SiOC Fibrous TPS Technology, Mr. Thomas Rosengren, MATECH 1415 - 1440 Bimetallic TPS Structure with Integrated Anti- Oxidation Coating, Dr. George Ritter, EWI 1440 – 1510 Break 1510 - 1535 Ceramic Truss Core Control Surface, Ms. Lee Anne Lehman, The Boeing Company 1535 - 1600 Tailorable Ceramic Micro-truss as a Panel Core Structure for Thermal Protection Systems, Dr. Daniel Driemeyer, The Boeing Company 1600 - 1625 Innovative Materials & Processes Development for Structurally Integrated Thermal Protection Systems, Ms. Kerry Hopp, Materials Research & Design, Inc. Planetary Orbit and Exploration Technologies continued New Nonflammable, High- Strength, Lightweight Structural Cryogenic Composite Material in Development, Ms. Katherine Rodway, XCOR Aerospace Deployable Articulating Array for Nanosatellites, Mr. Dan Turse, Composite Technology Development, Inc. Highly Conductive Graphite Thermal Strap Assemblies for Weight Savings in Thermal Management, Mr. Stephen Nieczkoski, Technology Applications, Inc. InAs/GaSb-based Barrier Architecture MWIR & LWIR Detectors for Space Applications, Dr. Vincent Cowan, AFRL Inflatable Re-entry Vehicle Experiment Technology Development and Demonstrator Flight Test, Dr. Anthony Calomino, NASA LaRC Development of Large Scale Hypersonic Inflatable Atmospheric Decelerators Development of Large Scale Hypersonic Inflatable Atmospheric Decelerators, Dr. Anthony Calomino, NASA LaRC Aging of Flexible TPS Materials, Jacues Cuneo, Southern Research Institute Space Access & Propulsion continued High Performance Green Propulsion for Improved Responsiveness and Reduced Life Cycle Cost, Mr. Stephen Beckel, ATK (Alliant Techsystems) Electro-formed Engineered Rhenium with Improved Mechanical Properties, Mr. Scott O'Dell, Plasma Processes, LLC Low-Cost, High- Performance Materials for In-Space Propulsion, Dr. Arthur Fortini, Ultramet Ceramic Matrix Composites for Propulsion Structures Applications, Mr. Mitch Petervary, The Boeing Company, Research & Technology Manufacturing Overview of a 2.4 Meter Composite Cryotank, Mr. Carlos Guzman, The Boeing Company Hydrogen Permeation Testing and Analysis for Composite Cryotanks, Mr. Michael Robinson, Boeing To Be Announced
1625 - 1650 Summary of Pre-Test Predictions and Post-Test Results for Structurally Integrated Thermal Protection System Joint Subelements, Mr. Daniel Howren, Materials Research & Design, Inc. Hypersonic Inflatable Decelerator Study, Dr. Suraj Rawal, Lockheed Martin Fiber Placement of an Out of Autoclave Tank Using Low cost Platforms, Mr. Brice Johnson, Boeing 1650 - 1900 Poster Session and Reception (Sponsored by Boeing) Thursday, 27 June 2013 0700 - 0745 Speaker Breakfast for Thursday Presenters 0700 - 0800 Attendee Continental Breakfast 0700 - 1530 Registration Concurrent Sessions Missiles & Missile Defense Session Organizers: Dr. Doug Deason, MDA; Mr. Gerald Russell, RDECOM; Mr. Mark Smith, AEDC; Mr. Paul Marchol, Aerojet; and Dr. Curtis Martin, NSWCCD Innovations in Materials Session Organizers: Dr. John Rivard, ORNL; Dr. Russ Lipeles, The Aerospace Corporation; Dr. Eric Wuchina, NSWC; Dr. Brian Holloway, DARPA; Dr. Anne Fischer, DARPA; and Dr. John Schmisseur, AFOSR Space Access & Propulsion continued 0800 - 0805 Session Intro Session Intro Session Intro 0805 - 0830 Technology Roadmap for Affordable and Producible EO/IR/RF Sensor Window Materials, Mr. Doug Freitag, USACA 0830 - 0855 UHT CMCs for Propulsion Applications, Mr. Steve Kirkwood, MATECH 0855 - 0920 Survivable Broadband Optical Coating for Ballistic Missile Defense Missions, Dr. Bill Goodman, Trex Enterprises Corporation 0920 - 0945 Powder Towpreg Process for Fabrication of High Temperature Composites, Dr. Ronald Allred, Adherent Technologies, Injection Moldable Pressureless Sintered Silicon Nitride, Mr. Mark Hawthorne, ATC Materials In Situ Processing of Lunar Glass Fiber and Composites, Dr. Edward Pope, MATECH Synthesis of Alloyed Nanocarbide/Graphene Nanocomposites by a Scalable Process, Dr. E.G. Baburaj, Clarkson Aerospace Corp. Mechanical Properties of Spark Plasma Sintered ZrB2 with Oxide Reducing Agents, Mr. David Pham, University of Arizona Compression Analysis and Test of Fluted-Core Sandwich Composite Panels, Dr. Marc Schultz, NASA LaRC Thin, Lightweight Aerogel Thermal Insulation for Space Applications, Dr. Shannon White, Aspen Aerogels, Inc. A Technical Evaluation of Additive Manufacturing Readiness for Rocket Engine Component Manufacturing, Mr. David Salazar, Sierra Lobo, Inc. Additive Manufactured Propulsion Systems Development Status and Applications, Mr. Christian Carpenter, Aerojet
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Page 3 and 4: Reentry Vehicles, Mr. Jean Doucette
Page 5: 0945 - 1015 Break Estimating Surfac
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2013 National Space & Missile Materials Symposium

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