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2012 National Space & Missile Materials Symposium

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Integrated Thermal<br />

Protection System Joint<br />

Subelement Test Articles,<br />

Mr. Daniel Howren,<br />

<strong>Materials</strong> Research &<br />

Design, Inc.<br />

1415 - 1440 Experimental Evaluation<br />

of Gap Thermal<br />

Resistance in a Hot<br />

Composite Structure,<br />

Mr. Brett Hauber, AFRL<br />

1440 – 1510 Break<br />

1510 - 1535 Innovative Core<br />

Development for<br />

Structurally Integrated<br />

Thermal Protection<br />

Systems,<br />

Mr. Craig Iwano, <strong>Materials</strong><br />

Research & Design, Inc.<br />

1535 - 1600 Ground Test Studies in the<br />

LENS Hypervelocity<br />

Tunnels of <strong>Missile</strong> and Re-<br />

Entry Vehicles at<br />

Duplicated Flight<br />

Conditions,<br />

Dr. Michael Holden,<br />

CUBRC<br />

1600 - 1625 Updating the Hypersonic<br />

Weather Encounter<br />

Ground Testing Capability<br />

of AEDC Range G,<br />

Mr. Richard Rushing,<br />

AEDC<br />

1625 - 1650 Manufacture and Testing<br />

of Niobium Alloy/Lithium<br />

Heat Pipes for Wing<br />

Leading Edges,<br />

Mr. John Rosenfeld,<br />

Adhesive Bonding<br />

Processes,<br />

Mr. Emmanuel Cua,<br />

Aerojet<br />

Comparison of Leak Rates<br />

of In-Flight and Ground<br />

Based Exposed Silicone<br />

Elastomer Seals,<br />

Ms. Janice Wasowski, The<br />

University of Akron<br />

A Computational Leak<br />

Rate Prediction Method<br />

for Elastomer <strong>Space</strong> Seals,<br />

Dr. Nicholas Garafalo, The<br />

University of Akron<br />

Preparation and Testing<br />

of Transparent<br />

Hyperbranched<br />

Polyhedral Oligomeric<br />

Silsesquioxane (HB-POSS)<br />

Nanostructured<br />

Protective Coatings and<br />

Adhesives for <strong>Space</strong><br />

Applications,<br />

Dr. Clare Hartmann-<br />

Thompson, Michigan<br />

Molecular Institute<br />

Material Classification<br />

and Damage Assessment<br />

Using Laser Polarimetry,<br />

Dr. Brian Hoover,<br />

Advanced Optical<br />

Damage Tolerance<br />

Behavior of Friction Stir<br />

Welds in Aluminum Alloys,<br />

Dr. Preston McGill, NASA<br />

MSFC<br />

HIAD Application<br />

Technology Benefits and<br />

Requirements for Future<br />

<strong>Space</strong> Mission Exploration<br />

Overview of TRL<br />

Development for<br />

Inflatable EDL<br />

Decelerators,<br />

Dr. Anthony Calomino,<br />

NASA LaRC<br />

Evaluation of Lightweight<br />

Radiator Fin Construction<br />

for High-Temperature<br />

Nuclear Electric Powered<br />

<strong>Space</strong>craft,<br />

Ms. Briana Tomboulian,<br />

University of<br />

Massachusetts Amherst<br />

Lightweight Nanomaterial<br />

Shielded Cables and<br />

Harnesses for <strong>Space</strong> and<br />

<strong>Missile</strong> Applications,<br />

Mrs. Megan Caprio, San<br />

Diego Composites, Inc.<br />

Remote UV Fluorescence<br />

Lifetime Imaging<br />

Spectrometer<br />

(RUVPhase)for the<br />

Scientific Investigation of<br />

Planetary Surface and<br />

Subsurface Geophysical<br />

Terrain, Dr. Edgar<br />

Mendoza, Redondo<br />

Optics, Inc.<br />

Interplanetary Heatshield,<br />

Mr. Mike Fuller, ATK

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