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Thursday, 28 June 2012<br />
0945 - 1015 BREAK (Grand Ballroom Foyer)<br />
1015 - 1040 Oxide Ceramic Matrix Composite (CMC) for<br />
Missile Radomes<br />
Mr. Steve Atmur, ATK – COI Ceramics, Inc.<br />
1040 - 1105 Development of Structural Insulators for MDA<br />
Applications<br />
Mr. Kent Buesking, Materials Research & Design, Inc.<br />
1105 - 1130 Integration of Thermal Interface Materials into<br />
Missile Airframe Structures<br />
Mrs. Carissa Russell, U.S. Army AMRDEC<br />
1130 - 1155 Non-Eroding Ceramic Nozzle Throat Insert<br />
Designs for Aluminized Propellant Solid Rocket<br />
Motor Applications<br />
Mr. Mike Fuller, ATK Aerospace Systems and<br />
Mr. Joseph Pluscauskis, Materials Research & Design,<br />
Inc.<br />
1155 - 1300 LUNCH BREAK (ON YOUR OWN)<br />
1300 - 1325 Ballistic Missile Defense Interceptor System<br />
Innovation Concepts and Strategy<br />
Mr. Andrew Facciano, Raytheon Missile Systems<br />
1325 - 1350 Determination of Design Allowables for Novoltex<br />
C-SiC<br />
Mr. Paul Marchol, Aerojet<br />
1350 - 1415 Comparison of GE 2D and 3D C-SiC Materials:<br />
Properties, Processing and Microstructure<br />
Mr. Randall Jenkins, Southern Research Institute<br />
1415 - 1440 Thermostructural Analysis of LHMEL Phenolic,<br />
Mr. Hans Jensen, Materials Research & Design, Inc.<br />
1440 - 1510 BREAK (Grand Ballroom Foyer)<br />
1510 - 1535 Demonstration of Segmented Heater Operation at<br />
Glide Vehicle Conditions<br />
Dr. Joseph Sheeley, ATA-AEDC<br />
1535 - 1600 NDE Methods for Filament Wound Aluminum<br />
Metal Matrix Composites<br />
Dr. Eric Johnson, The Aerospace Corporation<br />
1600 - 1625 Characterization of the Artificial Rain Environment<br />
at the Holloman High Speed Test Track<br />
Dr. Michelle Zeisset, 846th TS<br />
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