2012 National Space & Missile Materials Symposium
2012 National Space & Missile Materials Symposium
2012 National Space & Missile Materials Symposium
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0945 - 1015 Break<br />
Texas at Arlington<br />
1015 - 1040 Ultra High Temperature<br />
Mechanical Testing of<br />
ZrB2 Based Ceramics,<br />
Mr. Eric Neuman, Missouri<br />
University of Science &<br />
Technology<br />
1040 - 1105 Structural Performance of<br />
Continuous Core<br />
Structurally Integrated<br />
Thermal Protection<br />
System, Mr. Carl Poteet,<br />
NASA LaRC<br />
1105 - 1130 Energy Conversion<br />
Capabilities in Scramjet<br />
Vehicles Using<br />
Thermoelectrics,<br />
Mr. Kevin Yost, AFRL<br />
1130 - 1155 Overview of TRL<br />
Devlopments for Large<br />
Scale Atmopheric<br />
Inflatable Decelerators,<br />
Dr. Anthony Calomino,<br />
NASA LaRC<br />
1155 – 1300 Lunch Break<br />
Hypersonics<br />
continued<br />
1300 - 1325 NASA Fundamental<br />
Aeronautics Hypersonics<br />
Project Overview,<br />
Mr. Craig Stephens, NASA<br />
DFRC<br />
1325 - 1350 Low Cost Lightweight<br />
High-Speed Structures,<br />
Dr. Bill Garver, Lockheed<br />
Martin Aeronautics<br />
Company<br />
1350 - 1415 Results of Trade Study<br />
Design Analyses for<br />
Selection and Fabrication<br />
of Candidate Structurally<br />
Coverglasses for<br />
Advanced Photovoltaics,<br />
Mr. James Belcher,<br />
Infoscitex Corporation<br />
Mechanical Testing of<br />
Silicon Carbide<br />
Specimens on MISSE-7,<br />
Dr. David Witkin, The<br />
Aerospace Corporation<br />
Results of International<br />
<strong>Space</strong> Station Vehicle<br />
<strong>Materials</strong> Exposed on<br />
MISSE-7B,<br />
Mrs. Miria Finckenor, NASA<br />
MSFC<br />
<strong>Space</strong> Environmental<br />
Analysis, Deposition<br />
Analysis and Resistivity<br />
Analysis of Z-93C55 White<br />
Conductive Thermal<br />
Control Material System<br />
(TCMS),<br />
Mr. Michael Kenny, Alion<br />
Science & Technology<br />
<strong>Space</strong> <strong>Materials</strong><br />
Experiments &<br />
Environmental Effects<br />
Simulation<br />
continued<br />
Boeing / MISSE-8 On-Orbit<br />
Data First Results,<br />
Dr. Mark Clemen, Boeing<br />
Research & Technology<br />
Energy Considerations<br />
and Reaction Rates for<br />
Atomic Oxygen-Surface<br />
Collisions,<br />
Dr. Gary Pippin, The<br />
Boeing Company<br />
Application of Classical<br />
Surface Energy Theory to<br />
Quantify Rubber Surface<br />
Conditions to Support<br />
Composite Cryotank<br />
Technologies and<br />
Development Phase 2,<br />
Dan Rivera, The Boeing<br />
Company<br />
Test Approach to CCTD,<br />
Mr. Cataldo Mazzola, The<br />
Boeing Company<br />
C-C Nozzle Extension<br />
Designs and Analyses in<br />
Support of J-2X Nozzle<br />
Extension Risk Reduction<br />
Effort,<br />
Ms. Leslie Weller, <strong>Materials</strong><br />
Research & Design, Inc.<br />
Digital Material Skins: A<br />
Reversible, Reusable,<br />
Recyclable Pressure<br />
Vessel, Sarah Hovepian,<br />
The Massachusetts<br />
Institute of Technology,<br />
NASA <strong>Space</strong> Technology<br />
Research Fellowship<br />
<strong>Space</strong> Exploration<br />
continued<br />
NASA Composite Crew<br />
Module Manufacturing,<br />
Dawson Vincent, The<br />
Geocent Company<br />
Hydrocarbon Boost<br />
Technology<br />
Demonstration Program,<br />
Jamie Cleland, Aerojet<br />
LE-X Nozzle Liner<br />
Prototype Development,<br />
Mr. Guido Canzona, Pratt<br />
& Whitney Rocketdyne