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2013 National Space & Missile Materials Symposium

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Reentry Vehicles, Mr. Jean<br />

Doucette, Textron Defense<br />

Systems<br />

1400 - 1425 Thermal Insulation<br />

Performance of Aerogel<br />

Composites for Satellites,<br />

Dr. Nicholas Zafiropoulos,<br />

Aspen Aerogels, Inc.<br />

1425 - 1450 Hypersonic Propulsion, Mr.<br />

Chris Kogstrom, ATK<br />

1450 - 1515 Development and Analysis<br />

of Continuous SiC Fiber-<br />

Reinforced HfB2-SiC<br />

Composites for Hypersonic<br />

Flight Applications, Dr.<br />

Clifford Leslie, AFRL & NRC<br />

Research Associateship<br />

Program<br />

4-Meter Primary Reflector<br />

Demonstrator for the<br />

Scanning Microwave Limb<br />

Sounder, Mr. Eldon Kasl,<br />

Vanguard <strong>Space</strong><br />

Technologies, Inc.<br />

Development of PICA Gap<br />

Filler for Heatshield<br />

Assemblies, Dr. Steven<br />

Violette, Fiber <strong>Materials</strong><br />

Inc., Graftech<br />

International<br />

1515 - 1545 Root beer Float Break (Sponsored by Plasma Processes)<br />

1545 - 1610 Overview of <strong>National</strong><br />

Hypersonic Science<br />

Center for <strong>Materials</strong> and<br />

Structures, Dr. Dave<br />

Marshall, Teledyne<br />

The Impact of Thermally<br />

Induced Property Changes<br />

of PICA on Ultrasonic<br />

Ablation Thermometry, Mr.<br />

Joseph Lloyd, Industrial<br />

Measurement Systems, Inc.<br />

1610 - 1635 Woven TPS – Enabling<br />

Missions Beyond Heritage<br />

Carbon Phenolic, Dr.<br />

Margaret Stackpoole,<br />

NASA ARC<br />

1635 - 1700 MURI, Dr. Erica Corral,<br />

University of Arizona<br />

Viability of 3 D Woven<br />

Carbon Cloth and<br />

Advanced Carbon-<br />

Carbon Ribs for use in<br />

Adaptive Deployable Entry<br />

Placement Technology for<br />

Future NASA Missions, Dr.<br />

Ethiraj Venkatapathy,<br />

NASA Ames Research<br />

Center<br />

Sheila Thibeault, NASA<br />

LARC<br />

Design of Thermo-<br />

Structural Test for In-Plane<br />

Compression Fracture<br />

under High Thermal<br />

Gradients, Mr. Hans<br />

Jensen, <strong>Materials</strong><br />

Research & Design, Inc.<br />

Further Analysis of<br />

<strong>Materials</strong> Exposed on<br />

MISSE-7B, Mr. Michael<br />

Kravchenko, NASA MSFC<br />

<strong>Space</strong> Environmental<br />

Analysis, Resistivity<br />

Analysis and in-situ<br />

Deposition on <strong>Space</strong> X<br />

Dragon Trunks Using<br />

Mobile Deposition Unit, of<br />

Z-93C55 White Conductive<br />

Thermal Control Material<br />

System (TCMS), Mr.<br />

Michael Kenny, ALION<br />

Science and Technology<br />

Adhesion Forces of<br />

Silicone Elastomer Seals<br />

Pretreated with Atomic<br />

Oxygen, Dr. Heather<br />

Oravec, The University of<br />

Akron<br />

Use of Molecular<br />

Dynamics Simulations to<br />

Model <strong>Materials</strong> Damage<br />

Due to Hyperthermal<br />

Atomic Oxygen, Dr.<br />

Vanessa Oklejas, The<br />

Aerospace Corporation<br />

An Extensible Model for<br />

Environmental Effects in<br />

<strong>Space</strong> and Test Chambers,<br />

Dr. Jason Cline, Spectral<br />

Sciences, Inc.

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