no photographs permitted - advanced...

Draft Program REV#12 1/5/2015

39th Annual Conference on

Composites, Materials and Structures (U.S. Citizens Only / ITAR Restricted Sessions)

No Photographs Permitted

http://advancedceramics.org/CMS2015

http://advancedceramics.org/CMS2015


Program at a Glance Sunday Evening, January 25, 2015

6:00-9:00pm Pre-Registration (Convention Center Lobby)

Complimentary Refreshments

Monday, January 26, 2015 Tuesday, January 27, 2015

Morning Session 8:40-11:30 Plenary Session

Afternoon – Two (2) Concurrent Sessions 1:30-5:00 Session 1: Ceramic Matrix Composites 1 1:30-4:40 Session 2: Carbon-Carbon Composite Materials 1

Afternoon/Evening Activities Location: Pavilion

12:00-1:30 Exhibitor Set-up 5:00-7:00 ITAR Restricted Expo and Networking Social

Morning – Two (2) Concurrent Sessions 8:30-12:00 Session 1: Ceramic Matrix Composites 2 8:30-12:00 Session 2: Carbon-Carbon Composites Materials 2

Afternoon – Two (2) Concurrent Sessions 1:30-5:00 Session 1: Ceramic Matrix Composites 3 1:30-4:20 Session 2: Carbon-Carbon Composites Materials 3

Evening Activities Location: Pavilion

5:00-7:00 ITAR Restricted Expo and Networking Social 7:30-8:30 Exhibitor Breakdown

Wednesday, January 28, 2015 Thursday, January 29, 2015

Morning – Three (3) Concurrent Sessions 8:15-12:00 Session 1: Behavior and Life Ceramic Matrix

Composites 1 8:30-12:00 Session 2: Carbon-Carbon Composites Materials 4 8:30-12:00 Session 3: Extreme Environment Materials 1 -

Divert Propulsion Materials

12:00-1:30 Complimentary Radisson Luncheon (Pavilion) or Lunch on your own

Afternoon Session – Three (3) Concurrent Sessions

1:30-5:00 Session 1: Behavior and Life Ceramic Matrix

Composites 2 1:30-4:40 Session 2: Carbon-Carbon Composites Materials 5 1:30-5:40 Session 3: Extreme Environment Materials 2

Morning – Two (2) Concurrent Sessions 8:15-12:00 Session 1: Behavior and Life of Ceramic Matrix

Composites 3 8:30-10:40 Session 2: Hypersonic Materials 1

Afternoon Session – Two (2) Concurrent Sessions 1:30-5:00 Session 1: Behavior and Life of Ceramic Matrix

Composites 4 1:30-3:00 Session 2: Hypersonic Materials 2

Additional Activities at the Hotel

Wednesday: 5:00-6:30 CMH-17 Handbook Martinique Meeting Room (off hotel lobby)

Thursday: Noon-1:30 CMH-17 Handbook Jamaica Meeting Room (off hotel lobby)

Steve Atmur, ATK Space Systems, Rocket Center, WV Email: [email protected]

mailto:[email protected]


MONDAY MORNING – JANUARY 26, 2015 Plenary Session Location: Salons 1 and 2

7:30-8:30am Registration and Continental Breakfast 8:40-8:50am Welcome Remarks by Todd Steyer, USACA Chair 8:50-9:00am Opening Comments by Mark Opeka, Program Chair 9:00-9:40am SR71 Reconnaissance – The View from the Cockpit (tentative title)

General Buck Adams (AF Retired) 9:40-10:10am Hypersonic Flight: Molecular Simulation of Oxygen Reactions with Realistic Silica and Carbon

Surfaces at High Temperature Dr. Thomas Schwartzentruber, University of Minnesota, Minneapolis, MN

10:10-10:30am BREAK 10:30-11:00am Title TBD

Greg Becker, Head of Program, CMCs, Rolls-Royce Corporation, Indianapolis, IN 11:00-11:30am Speaker 4 – Tentative, Orion Program Office TBD


MONDAY AFTERNOON – JANUARY 26, 2015 Session 1: Ceramic Matrix Composites 1 Session Chairs: Dennis Fox and J. Douglas Kiser, NASA Glenn Research Center, Cleveland, OH Location: Salon 2

1:35-1:40pm Session Chairs Remarks 1:40-2:00pm Creep and Fatigue Characterization of 3D SiC/SiC Composites with (CVI+PIP) Hybrid Matrix

R. Bhatt and J. DiCarlo, NASA Glenn Research Center, Cleveland, OH 2:00-2:20pm Creep Behavior and Durability of Cracked CMC

R. Bhatt, D. Fox and C. Smith, NASA Glenn Research Center, Cleveland, OH 2:20-2:40pm Silicide-based Matrix Development for 1482°C Application

S. Raj, NASA Glenn Research Center, Cleveland, OH 2:40-3:00pm An Evaluation of the Performance of CMC Material for a Cooled Vane in a Small Engine

J. Lang and R. Bhatt, NASA Glenn Research Center, Cleveland, OH 3:00-3:20pm BREAK 3:20-3:40pm Analysis and Design of a Thin Panel Cruciform Specimen for High Temperature Biaxial Testing

of Ceramic Matrix Composites L. Weller and B. Sullivan, Materials Research & Design, Inc., Wayne, PA

3:40-4:00pm Experimental Evaluation of Foreign Object Damage Resistant Ceramic Matrix Composites

C. Iwano, E.J. Klock-McCook and B. Sullivan, Materials Research & Design, Inc., Wayne, PA J. Cuneo and J. Koenig, Southern Research Institute, Birmingham, AL

4:00-4:20pm Elevated Temperature Ceramic Matrix Composite Fracture Toughness Testing

C. Iwano and B. Sullivan, Materials Research & Design, Inc., Wayne, PA J. Cuneo and J. Koenig, Southern Research Institute, Birmingham, AL

4:20-4:40pm Design and Analysis of 3D Braided CMC Fasteners

D. Caputo and K. Buesking, Materials Research & Design, Inc., Wayne, PA H. Lam and B. Ong, DE Technologies, King of Prussia, PA

4:40-5:00pm 3-Dimensionally Braided Preform for Ceramic Matrix Composites

H. Lam, B. Ong, E. Yelk, R. Colbert and W. Flis, DE Technologies, King of Prussia, PA


MONDAY AFTERNOON – JANUARY 26, 2015 Session 2: Carbon-Carbon Composite Materials 1 Session Chairs: Andrew Swanson, Air Force Research Laboratory, Wright Patterson AFB, OH

Michelle Pizzo, NASA Langley Research Center, Hampton, VA Location: Salon 1

1:35-1:40pm Session Chairs Remarks 1:40-2:20pm Falcon Program Executive Summary

C. Pagoda, Lockheed Martin Space Systems Company, King of Prussia, PA 2:20-2:40pm Falcon Aeroshell Design Overview

D. Hecht, Lockheed Martin Aeronautics Company, Fort Worth, TX 2:40-3:00pm A Manufacturing Perspective of Falcon C-C

A. Brown, C-CAT, Kennedale, TX 3:00-3:20pm BREAK 3:20-4:00pm Falcon 2-D Carbon-Carbon Material Property Testing Overview

D. Lordan and G. McNelis, Lockheed Martin Space Systems Company, King of Prussia, PA A. Williams, Southern Research Institute, Birmingham, AL

4:00-4:20pm Falcon 2-D Carbon-Carbon Material Property Testing Summary and Lessons Learned

C. Pagoda, Lockheed Martin Space Systems Company, King of Prussia, PA 4:20-4:40am Non-Destructive Evaluation Techniques and Observations for 2D Carbon-Carbon

D. Lordan, Lockheed Martin Space Systems Company, King of Prussia, PA G. Daspit, Southern Research Institute, Birmingham, AL


MONDAY EVENING – JANUARY 26, 2015

12:00-1:30pm Exhibitor Set-up

5:00-7:00pm ITAR RESTRICTED Expo and Networking Social

LIST OF EXHIBITORS • C-CAT • Cincinnati Testing • COI Ceramics, Inc. • EEMS, LLC • Element Materials Technology • Free Form Fibers • GE Aviation • Lancer Systems • Materials Research & Design, Inc. • MATECH • Plasma Processes • Starfire Systems, Inc. • Ultramet • Zircar Zironia, Inc.


Exhibitors Guide

Company

Company Profile Booth

Number Plasma Processes Plasma Processes specializes in the development and manufacture of high

temperature materials, coatings and additive manufacturing components &

powders. We develop, apply and validate coating solutions for thermal and

oxidation protection, emissivity, wear and corrosion resistance and dimensional

restoration, in addition to the additive manufacture of net-shape components by

vacuum plasma and EL-Form® deposition processes. We offer advanced materials

support to a wide variety of industries.

100

Zircar Zirconia, Inc. For more than 40 years, providing custom insulation solutions for applications up to

2400 Celsius. Manufacturer of alumina, ceria, hafnia and ytrria stabilized zirconia

fiber insulation including boards, blankets, cylinders, discs and textiles. Custom

machining and assembly offered. 1600C and 1700C Lab Furnaces operating on

110V are in stock.

101

Carbon-Carbon Advanced Technologies

Carbon-Carbon Advanced Technologies, Inc. Pioneering High Temperature

Carbon-Carbon composites; deliverable for Flight Programs and Space

technologies.

102

Ultramet Ultramet is an ISO 9001:2008-certified producer of flight-qualified components,

comprised of engineers, scientists and support personnel, production and R&D

facilities particularly suited to the research, development and production of

advanced materials including high temperature capability, corrosion- and erosion-

resistant materials. Ultramet personnel will be available to discuss your specific

materials-related applications.

103

Lancer Systems Lancer engineers innovation that improves. As an engineering and manufacturing

firm, we create value solutions for challenging and harsh environment applications

using composite, ceramic and fiber optic technologies, with capabilities that span

across our advanced weapons & components, composites and fiber optics business

areas. We're proud to be trusted by customers in the defense, aerospace, natural

gas and oil industries www.Lancer-Systems.com.

104

EEMS, LLC EEMS, LLC is a technology company enabling extreme environment materials

solutions through the supply of polymers, resins and related materials that enable

manufactures to create products that are able to run hotter, last longer and are

lighter.

105

Cincinnati Testing Labs

106

http://www.lancer-systems.com/


Company

Company Profile

Booth Number

MATECH MATECH has developed and produces 500 filament ceramic fiber tow of two types

of silicon-based fibers, silicon nitride/carbide (SiNC-1400X) and stoichiometric

silicon carbide (SiC-1900X) for use in advanced ceramic matrix composites (CMCs).

MATECH is a leader in ultra-high-temperature (UHT) CMCs for missile propulsion

and aerothermal TPS applications. MATECH manufactures UHT C/ZrOC CMCs.

MATECH manufactures SiC-matrix CMCs by PIP, CVI, Hybrid CVI/PIP and FAST

CMC processing. MATECH has a dedicated CVI/CVD facility for both interface

coatings and matrix densification. MATECH has a dedicated weaving lab

specializing in high modulus ceramic fibers. MATECH is fully integrated, from the

manufacture of fibers, weaving of fabric, deposition of interface coatings and CMC

densification.

107

Starfire Systems, Inc. Starfire Systems, Inc (SSI) is a specialty material company focused on Polymer

Derived Ceramics (PDC) and its Polymer-to-Ceramic TM technology. SSI's core

business is synthesis of silicon-based pre-ceramic polymers and SOL-GEL derived

oxide forming materials which are used in polymer matrix composites, oxide and

non-oxide ceramic matrix composite fabrication. SSI's high temperature materials

are useful in a variety of applications where durable, lightweight and high

temperature ceramics or coatings are required, such as frictional components,

electronic components, thermal protection systems and rocket nozzles. As a raw

material and technology system supplier, SSI continues to focus on supporting our

manufacturing partners to develop materials and systems that meet the needs of a

broader range of customers and end markets.

200

Element Materials Technology

An industry leader in evaluating materials, components and devices for over 40

years. We are a mechanical testing laboratory with particular expertise in elevated

temperature, low-cycle fatigue testing. In addition, we offer high-quality monotonic

testing services, including tension and compression, torsion, fracture mechanics,

stress and creep rupture.

201

202

GE Aviation GE Aviation is a world-leading provider of jet and turboprop engines, components

and integrated systems for commercial, military, business and general aviation

aircraft and ship propulsion applications. GE Aviation has a global service network

to support these offerings.

203

COI Ceramics, Inc. COI Ceramics, Inc. (COIC) an ATK Affiliate Company is a premiere supplier of

Ceramic Matrix Composite (CMC) materials for aerospace, defense and industrial

applications. A complete range of both oxide and carbide CMC materials provides

customers with the best performance solution for each unique application, including

aircraft exhaust systems, high-temperature missile radomes and honeycomb

assemblies for thermal protection systems and structural applications.

204


Company

Company Profile

Booth Number

205

Free Form Fibers Free Form Fibers (FFF) is the sole producer of laser-printed Silicon Carbide (SiC)

and Boron Carbide fibers in the world. FFF's unique process harnesses the flexibility

of additive manufacturing (AM) and the purity of Chemical Vapor Deposition (CVD)

in a highly flexible production process for multiple monofilaments. Filament

diameters can be customized from 15 to 80 micron and so can their chemical

composition. For example, the LP-20SC line of Silicon Carbide is comprised of up to

300 continuous filaments, 20 microns in diameter and of CVD-quality composition.

Our unique direct fiber laser printing technology requires no core and produces

arrays of filaments that we have demonstrated can be coated with a layer of Boron

Nitride and subsequently coated with SiC. Fibers can be made available in tapes of

parallel monofilaments or in tows of continuous filaments appropriately sized for

CMC applications.

206

Materials Research & Design, Inc.

Materials Research & Design (MR&D) is a small business that provides research

and design services to the aerospace materials community. Typical programs at

MR&D focus on the simultaneous design of material and structure to optimize

component cost, weight, or structural performance. Additional areas of interest focus

upon research into the behavior of composite materials and the development of

micromechanical models to analyze and understand observed properties. The

analytical approach employed by MR&D is based upon a practical understanding of

engineering issues founded upon a strong background of theoretical mechanics.

207


TUESDAY MORNING – JANUARY 27, 2015 Session 1: Ceramic Matrix Composites 2 Session Chairs: Mike Cinibulk, Air Force Research Laboratory, Wright Patterson AFB, OH Dennis Fox, NASA Glenn Research Center, Cleveland, OH Location: Salon 2

7:30-8:30am Registration and Continental Breakfast 8:35-8:40am Session Chairs Remarks 8:40-9:00am SiCf/SiC-HfB2 Composites for High Aerothermal Heating Applications

C. Carney, E. Jones and M. Cinibulk, Air Force Research Laboratory, Wright Patterson AFB, OH C. Leslie, UES, Inc., Dayton, OH J. Pierce, University of Dayton Research Institute, Dayton OH

9:00-9:20am Processing Modeling of Ceramic Matrix Composites

G. Wilks, Air Force Research Laboratory, Wright Patterson AFB, OH 9:20-9:40am Modeling of Polymer Impregnation and Pyrolysis Process for Ceramic Matrix Composites

U. Santhosh and J. Ahmad, Structural Analytics, Inc., Carlsbad, CA Y. Gowayed, Auburn University, Auburn, AL A. Szweda, COI Ceramics, Inc., San Diego, CA G. Ojard, United Technologies Research Center, East Hartford, CT R. Hall, Air Force Research Laboratory, Wright Patterson AFB, OH

9:40-10:00am Advanced Testing Techniques for Ceramic Matrix Composites

R. Bentley, Test Devices, Inc., Hudson, MA 10:00-10:20 BREAK 10:20-10:40am CVD-Inherited Properties of Laser-Printed Silicon Carbide Filaments

J. Pegna, S. Harrison, R. Goduguchinta, K. Williams and J. Schneiter, Free Form Fibers, Saratoga Springs, NY

10:40-11:00am Thermal Analysis Method for Multilayer Ceramic Composite Fuel Cladding

C. Parker and G. Markham, Ceramic Tubular Products, LLC, Rockville, MD 11:00-11:20am Improved Attachment Design for Ceramic Turbine Blades via Hybrid Concepts

M. Nathal, J. Gayda and I. Miller, N&R Engineering, Cleveland, OH 11:20-12:00 Update on CMH-17 Volume 5-Ceramic Matrix Composites: I) Materials and Processes Working

Group and II) Testing Working Group K. David and W. Keith, The Boeing Company, Huntington Beach, CA J. Pierce, University of Dayton Research Institute, Dayton, OH J. D. Kiser, NASA Glenn Research Center, Cleveland, OH G. Wilson, GE Aviation, Cincinnati, OH

12:00-1:30pm Lunch on your own


TUESDAY MORNING – JANUARY 27, 2015 Session 2: Carbon-Carbon Composite Materials 2 Session Chairs: Andrew Swanson, Air Force Research Laboratory, Wright Patterson AFB, OH

Michelle Pizzo, NASA Langley Research Center, Hampton, VA Location: Salon 1

7:30-8:30am Registration and Continental Breakfast 8:35-8:40am Session Chairs Remarks 8:40-9:00am Interlaminar Shear Testing of Falcon 2D Carbon-Carbon

K. Witmer, Lockheed Martin Space Systems Company, King of Prussia, PA 9:00-9:20am Design of a Double Notch Shear Strength Specimen for Falcon HTV-2 C-C Material with B-studs

D. Howren, K. Hopp and B. Sullivan, Materials Research & Design, Inc., Wayne, PA 9:20-9:40am Effect of Test Specimen Shape and Size on Interlaminar Tensile Properties of Advanced

Carbon-Carbon Composites W. Vaughn, NASA Langley Research Center, Hampton, VA Z. Simms, Utah State, Logan, UT

9:40-10:00am Design Analysis of Annular Interlaminar Tensile Strength Specimen for C-C Materials

K. Hopp, C. Mackie, M. Robinson and B. Sullivan, Materials Research & Design, Inc., Wayne, PA J. Cuneo and J. Koenig, Southern Research Institute, Birmingham, AL

10:00-10:20am BREAK 10:20-10:40am Interlaminar Tension and Shear Comparisons Between ACC-6 Vintages and Techniques

J. Cuneo and J. Koenig, Southern Research Institute, Birmingham, AL 10:40-11:00am Advanced Matrix Carbon-Carbon for Ablation Inhibition

A. Vecera, C-CAT, Kennedale, TX 11:00-11:20am Mode I Fracture Toughness Specimen Design for Falcon HTV C-C Materials With and Without

B-stud Reinforcements M. Dion and B. Sullivan, Materials Research & Design, Inc., Wayne, PA V. Rice, Lockheed Martin Space Systems Company, King of Prussia, PA

11:20-11:40am Falcon 2DCC Mode 1 and Mode 2 Fracture Toughness Results and Observations

J. Cuneo and J. Koenig, Southern Research Institute, Birmingham, AL M. Dion, B. Sullivan, K. Hopp and C. Mackie, Materials Research & Design, Inc., Wayne, PA V. Rice, G. McNelis and C. Pagoda, Lockheed Martin Space Systems Company, King of Prussia, PA D. Glass, NASA Langley Research Center, Hampton, VA

11:40-12:00pm Post-test Data Correlation Analysis of Curved Beam Test Specimen

K. Hopp, D. Howren, D. Furth and B. Sullivan, Materials Research & Design, Inc., Wayne, PA 12:00-1:30pm Lunch on your own


TUESDAY AFTERNOON – JANUARY 27, 2015 Session 1: Ceramic Matrix Composites 3 Session Chair: Dennis Fox, NASA Glenn Research Center, Cleveland, OH Location: Salon 2

1:35-1:40pm Session Chair Remarks 1:40-2:00pm Evaluation of CVI SiC/SiC Composites for High Temperature Turbine Engine Applications

J. D. Kiser, J. DiCarlo, L. Evans, R. Bhatt, R. Phillips and T. McCue, NASA Glenn, Cleveland, OH 2:00-2:20pm A Status Update and the Path to a 2700°F Capable CMC System

K. Newton and D. Berczik, Pratt & Whitney, East Hartford, CT T. Easler, ATK/COI Ceramics, San Diego CA

2:20-2:40pm Advanced MI CMC

G. Kirby, J. Steibel, M. Verrilli and H. Yun, GE Aviation Cincinnati, OH G. Corman, GE Global Research, Niskayuna, NY

2:40-3:00pm Progress and Plans for CMC Research at NASA Glenn in 2015

J. Grady, NASA Glenn Research Center, Cleveland, OH 3:00-3:20pm BREAK 3:20-3:40pm Vibration Testing of a Full Scale Oxide/Oxide Ceramic Matrix Composite (CMC) Exhaust Mixer

J. D. Kiser and J. Szelagowski, NASA Glenn Research Center, Cleveland, OH J. Sokhey and Tab Heffernan, Rolls-Royce North American Technology Inc., Indianapolis, IN J. Riedell, ATK COI Ceramics, San Diego, CA S. Atmur, ATK COI Ceramics, Rocket Center, WV T. Wyen, Air Force Research Laboratory, Wright Patterson AFB, OH J. Ursic, ZIN Technologies (at NASA GRC), Cleveland, OH

3:40-4:00pm CLEEN Flight Test of an Acoustic Ceramic Matrix Composite Primary Exhaust

M. Petervary, C. Frankel, T. Pinney, W. Keith, L. Lehman and B. Smith, The Boeing Company, Huntington Beach, CA

4:00-4:20pm On Modeling Damage and Failure Starting at Notches in Ceramic Matrix Fiber Reinforced

Composites A. Waas, University of Michigan, Ann Arbor, MI

4:20-4:40pm Field Assisted Sintering Technology (FAST) Densification of 2700°F SiC-SiC CMCs

E. Pope and K. Ringled, MATECH, Westlake Village, CA 4:40-5:00pm Advanced Ceramic Manufacturing & Machining Process Development - GEA-Army ManTech

Program M. Peretti, GE Aviation, Newark, DE


TUESDAY AFTERNOON – JANUARY 27, 2015 Session 2: Carbon-Carbon Composites Materials 3 Session Chair: Chris Tomko and Mark Jones, Naval Surface Warfare Center, Dahlgren, Dahlgren,

VA Location: Salon 1

1:35-1:40pm Session Chairs Remarks 1:40-2:00pm Delamination Parameters for Analysis of Hot Structures

N. Altobelli, Lockheed Martin Space Systems Company, King of Prussia, PA 2:00-2:20pm Rapid Thermal Expansion of Falcon 2-D Carbon-Carbon

V. Rice, Lockheed Martin Space Systems Company, King of Prussia, PA B. Patel, Southern Research Institute, Birmingham, AL

2:20-2:40pm Development and Testing of High Thermal Transient Modulus Facility

C. Appling and J. Koenig, Southern Research Institute, Birmingham, AL V. Rice and G. McNelis, Lockheed Martin Space Systems Company, King of Prussia, PA

2:40-3:00pm Creep Compression and Load Unload Reload

V. Rice, Lockheed Martin Space Systems Company, King of Prussia, PA 3:00-3:20pm BREAK 3:20-3:40pm Examination of Test Methods for Inducing In-Plane Compressive Strength Failure Under

Thermal Loading B. Sullivan and H. Jensen, Materials Research & Design, Inc., Wayne, PA

3:40-4:00pm RT Strain Visualization and Elevated Temperature Results of Tension and Compression of

Falcon 2-D Carbon-Carbon Material with and without B-Studs C. Moss and J. Cuneo, Southern Research Institute, Birmingham, AL

4:00-4:20pm Using Optimal Experimental Design to Improve Testing Procedures

W. Barger, University of Washington, Seattle, WA L. Green and D. Glass, NASA Langley Research Center, Hampton, VA


TUESDAY EVENING – JANUARY 27, 2015

5:00-7:00pm ITAR RESTRICTED Expo and Networking Social

7:30-8:30pm Exhibitor Breakdown


WEDNESDAY MORNING – JANUARY 28, 2015 Session 1: Behavior and Life Ceramic Matrix Composites 1 Session Chairs: Craig Przybyla and Larry Zawada, Air Force Research Laboratory, Wright

Patterson AFB, OH Jennifer Pierce, University of Dayton Research Institute, Dayton, OH

Location: Salon 1 7:30-8:30am Registration and Continental Breakfast 8:15-8:20am Session Chairs Remarks Workshop on Certification of Ceramic Matrix Composite Components for Aerospace Applications 8:20-8:50am Certification of Ceramic Matrix Composites for Military Engines

P. Bascom, Air Force Life Cycle Management Center, Wright Patterson AFB, OH 8:50-9:00am DISCUSSION 9:00-9:30am Ceramic Matrix Composite Challenges and Opportunities

M. Petervary and T. Steyer, The Boeing Company, Huntington Beach, CA 9:30-9:40am DISCUSSION 9:40-10:00am BREAK 10:00-10:30am Product Insertion – Lessons Learned

S. Atmur, ATK COI Ceramics, Rocket Center, WV S. Richardson and J. Paretti, ATK COI Ceramics, San Diego, CA

10:30-10:40am DISCUSSION 10:40-11:10am Qualification/Certification of SiC/SiC CMC Components for Military/Commercial Applications

M. Noe, D. Carper and S. Finn, GE Aviation, Evendale, OH 11:10-11:20am DISCUSSION 11:20-11:50am Federal Aviation Administration (FAA) Airworthiness Certification the Process and the

Challenge for CMC Components in Commercial Aircraft S. Gonczy, Gateway Materials Technology, Mt. Prospect, IL

11:50-12:00pm DISCUSSION 12:00-1:30pm Complimentary Radisson Luncheon (Pavilion)

or Lunch on your own


WEDNESDAY MORNING – JANUARY 28, 2015 Session 2: Carbon-Carbon Composite Materials 4 Session Chair: Chris Tomko and Michael Richards, Naval Surface Warfare Center, Dahlgren,

Dahlgren, VA Location: Salon 2

7:30-8:30am Registration and Continental Breakfast 8:35-8:40am Session Chairs Remarks 8:40-9:00am HTV-2 Aeroshell Prototype Structural Load Test

D. Hecht, Lockheed Martin Aeronautics Company, Fort Worth, TX 9:00-9:20am Ground Testing of Falcon 2D Carbon-Carbon in High Heat Flux Environments

R. Anthony, J. Piccini and K. Witmer, Lockheed Martin Space Systems Company, King of Prussia, PA 9:20-9:40am Falcon Aeroshell Horseshoe Feature Thermostructural Test

T. Bitzer, Lockheed Martin Space Systems Company, King of Prussia, PA 9:40-10:00am LHMEL 4 Point Bend Test of Falcon 2-D Carbon-Carbon

K. Witmer, Lockheed Martin Space Systems Company, King of Prussia, PA 10:00-10:20am BREAK 10:20-10:40am Assembly Joint Test Analytical Correlation

T. Bitzer, Lockheed Martin Space Systems Company, King of Prussia, PA 10:40-11:20am Thermo-Mechanical Testing of Carbon-Carbon for High Speed Applications

A. Swanson and J. Gauvin, Air Force Research Laboratory, Wright Patterson AFB, OH V. Goyal, J. Rome, S. Lukyanets and S. Frolik, Aerospace Corporation, El Segundo, CA

11:20-11:40am Thermal-Vibration Testing of High Temperature Thermocouple Plug

J. Feie, Air Force Research Laboratory, Wright Patterson AFB, OH 11:40-12:00pm Estimation of Surface Temperature and Heat Flux Values from Internal Temperature

Measurements Using Inverse Heat Transfer Methods M. Pizzo, NASA Langley Research Center, Hampton, VA

12:00-1:30pm Complimentary Radisson Luncheon (Pavilion)



WEDNESDAY MORNING – JANUARY 28, 2015 Session 3: Extreme Environment Materials 1 – Divert Propulsion Materials Session Chairs: Tim Dominick, ATK Missile Defense and Controls, Elkton, MD

Robert Haack, Missile Defense Agency, Huntsville, AL Location: Jamaica Meeting Room (off hotel lobby)

7:30-8:30am Registration and Continental Breakfast 8:35-8:40am Session Chairs Remarks 8:40-9:00am Evaluation and Future Direction for CMC Materials in Solid Propulsion Control Systems

T. Dominick, J. Higginson, A. Naramore, M. Porter, K. Schoonover and B. Sutton, ATK Missile Defense and Controls, Elkton, MD

9:00-9:20am Development and Demonstration of a CMC Material System for Attitude Control System

Applications K. Meiler, M. Levesque and M. Lippold, Fiber Materials, Inc., Biddeford, ME

9:20-9:40am LHMEL Testing of Candidate Structural Insulator Materials

R. Hein, T. Dominick and J. Steele, ATK Missile Defense and Controls, Elkton, MD G. Wendel and K. Kersker, ATK Launch Systems, Brigham City, UT

9:40-10:00am Integrated SiC & Re Coated C/ZrOC UHT Throat-Insulator Components for Enhanced Erosion

Resistance in DACS Environments T. Rosengren, S. Grandi, S. Kirkwood and E. Pope, MATECH, Westlake Village, CA D. Butts and A. Shchetkovskiy, Plasma Processes LLC, Huntsville, AL M. Porter, K. Schoonover and T. Dominick, ATK Missile Defense and Controls, Elkton, MD

10:00-10:20am BREAK 10:20-10:40am Ceramic Matrix Composite Structural Insulator Testing for SDACS Applications

T. Stewart and J. Brockmeyer, Ultramet, Pacoima, CA T. Dominick, M. Porter, A. Naramore and K. Schoonover, ATK Missile Defense and Controls, Elkton, MD

10:40-11:00am Aerogel-Filled Foam Insulating Structure Testing for SDACS Applications

T. Stewart and J. Brockmeyer, Ultramet, Pacoima CA T. Dominick, M. Porter, A. Naramore and K. Schoonover, ATK Missile Defense and Controls, Elkton, MD

11:00-11:20am Carbon Aerogels for Structural Insulation in DACS

W. Rhine, Aspen Aerogels, Inc., Northborough, MA 11:20-11:40am Low-Cost Refractory Metal-Lined Graphite and Carbon-Carbon Composites for Advanced SDACS

and LDACS V. Arrieta, S. Brown and B. Williams, Ultramet, Pacoima, CA K. Asoo, Digital Solid State Propulsion, Reno, NV

11:40-12:00pm High Performance Composite Joints for DACS Thrusters

E. Savrun and L. Lee Sienna Technologies, Inc., Seattle, WA D. Gerstner, Naval Surface Warfare Center, Carderock, West Bethesda, MD

12:00-1:30pm Complimentary Radisson Luncheon (Pavilion)



WEDNESDAY AFTERNOON – JANUARY 28, 2015 Session 1: Behavior and Life Ceramic Matrix Composites 2 Session Chairs: Craig Przybyla and Larry Zawada, Air Force Research Laboratory, Wright


Location: Salon 1 1:35-1:40pm Session Chairs Remarks 1:40-2:00pm Behavior and Life Prediction of SiC/SiC CMCs for Turbine Applications

B Cox and D. Marshall, Teledyne Scientific and Imaging Company, LLC, Thousand Oaks, CA T. Parthasararthy, UES Inc., Dayton, OH R. Ritchie, University of California, Berkeley, CA M. Vinup and N. Wali, Honeywell Inc., Phoenix, AZ Q. Yang, CompositeMore, Inc., Coral Gables, FL

2:00-2:20pm Progress on Damage and Delamination Modeling in SiC/SiC Ceramic Matrix Composites

R. Kumar and G. V. Srinivasan, United Technologies Research Center, East Hartford, CT K. Rugg, Pratt & Whitney, East Hartford, CT Z. Yuan and J. Fish, Multiscale Design System, LLC, New York, NY

2:20-2:40pm Multiscale Damage Propagation Methodology Development

G. Wilson, GE Aviation, Cincinnati, OH 2:40-3:00pm Modeling Environmental Damage of SiC/SiC CMCs

J. Shi, Rolls-Royce North America, Indianapolis, IN 3:00-3:20pm BREAK 3:20-4:00pm KEYNOTE: Constituent Effects on the Intrinsic Life of 2700oF SiC/SiC CMC

J. DiCarlo, NASA Glenn Research Center, Cleveland, OH R. Bhatt, Ohio Aerospace Institute, Cleveland, OH

4:00-4:20pm Developments in Physics Based Approach to Modeling Oxide CMC Response within ICME

Framework A. Bhattacharya and M. Petervary, The Boeing Company, Huntington Beach, CA

4:20-4:40pm Development of Computational Discrete Damage Modeling Package for CMCs

M. Braginsky, E. Zhou and E. Iarve, University of Dayton Research Institute, Dayton, OH C. Przybyla, Air Force Research Laboratory, Wright Patterson AFB, OH

4:40-5:00pm Effect of Microstructural Features and Properties of Constituents on the Thermo-Elastic

Properties of CMCs Y. Gowayed, Auburn University, Auburn, AL J. Pierce and D. Buchanan, University of Dayton Research Institute, Dayton, OH R. John and L. Zawada, Air Force Research Laboratory, Wright Patterson AFB, OH


WEDNESDAY AFTERNOON – JANUARY 28, 2015 Session 2: Carbon-Carbon Composite Materials 5 Session Chairs: Andrew Swanson, Air Force Research Laboratory, Wright Patterson AFB, OH

Craig Ohlhorst, NASA Langley Research Center, Hampton, VA Location: Salon 1

1:35-1:40pm Session Chairs Remarks 1:40-2:00pm Test Development and Determination of Effective Stress Due to Pore Pressure (alpha)

J. Hawbaker, J. Koenig, A. Cain and G. Daspit, Southern Research Institute, Birmingham, AL R. Sullivan and E. Baker, NASA Glenn Research Center, Cleveland, OH

2:00-2:20pm Measurements of Internal Pressure of Carbon-Carbons as a Function of High Heat Flux Heating

at LHMEL A. Cain, J. Hawbaker, G. Daspit and J. Koenig, Southern Research Institute, Birmingham, AL B. Sullivan, Materials Research & Design, Inc., Wayne, PA

2:20-2:40pm 2- D Carbon-Carbon Recession Testing Overview

B. Pye, Lockheed Martin Space Systems Company, King of Prussia, PA 2:40-3:00pm Oxidation Testing of Graphite and Carbon-Carbon for Kinetic Model Assessment

T. Risch and C. Kostyk, NASA Armstrong Flight Center, Edwards, CA 3:00-3:20pm BREAK 3:20-3:40pm HTV-2 Carbon Kinetics Sensitivity Analysis

T. Risch and C. Kostyk, NASA Armstrong Flight Center, Edwards, CA 3:40-4:00pm HTV-2 Leading Edge Arcjet Testing

D. Hecht, Lockheed Martin Aeronautics Company, Fort Worth, TX 4:00-4:20pm Falcon Aeroshell Horseshoe Feature Arcjet Testing

M. Britton, Lockheed Martin Space Systems Company, King of Prussia, PA 4:20-4:40pm NASA Ames PTF Recession Assessment of Falcon HTV-2 2DCC

D. Hudson, Leidos, Valley Forge, PA


WEDNESDAY AFTERNOON – JANUARY 28, 2015 Session 3: Extreme Environment Materials 2 Session Chairs: Joseph Pluscauskis, Materials Research & Design, Inc., Wayne, PA

Gautham Ramachandran, Lockheed Martin Aerospace, Sunnyvale CA Location: Jamaica Meeting Room (off hotel lobby)

1:40-2:00pm Non-Eroding Throat Insert: Design, Analysis, Fabrication and Testing

J. Pluscauskis, G. M. Tiscia and K. Buesking, Materials Research & Design, Inc., Wayne, PA D. Butts, G. Thom and T. McKechnie, Plasma Processes, LLC, Huntsville, AL N. Anderson, J. Fischer, G. Allen, B. Goldstone, T. Dominick, C. Carr, D. Bidwal, D. Axtell, C. Isaac, M. Porter, J. Porter, J. Lizardo and K. Moyes, ATK Missile Defense and Controls, Elkton MD J. Shigley, ATK Aerospace Group, Brigham City, UT

2:00-2:20pm Understanding Phase Stability in the Transition Metal Group IVB and VB Carbides

X. Yu and G. Thompson, University of Alabama, Tuscaloosa, AL C. Weinberger, Drexel University, Philadelphia, PA

2:20-2:40pm HfC based UHTC Composites for the Next Generation Hypersonic Vehicles

H. D. Lee, UES, Inc., Dayton, OH L. Matson, Air Force Research Laboratory, Wright Patterson AFB, OH

2:40-3:00pm Materials in Extreme Dynamic Environments Collaborative Research Alliance (MEDE CRA)

V. Nakano, Hopkins Extreme Materials Institute, Johns Hopkins University, Laurel, MD 3:00-3:20pm BREAK 3:20-3:40pm Aerogel-Filled Foam Core Insulation for Cryogenic Propellant Storage

V. Arrieta, B. Williams and S. Brown, Ultramet, Pacoima, CA B. Sullivan and L. Weller, Materials Research & Design, Inc., Wayne, PA M. Droege and S. Downey, Ocellus, Livermore, CA

3:40-4:00pm Microstructure and Hardness in Hot Pressed and Vacuum Plasma Sprayed HfB2-SiC

K. Vinson and G. Thompson, University of Alabama, Tuscaloosa, AL D. Butts, Plasma Processes, LLC, Huntsville, AL

4:00-4:20pm SiC-Based Fiber-Embedded Functional Microsystems: Nuclear Ceramics

J. Pegna, S. Harrison, R. Goduguchinta, K. Williams and J. Schneiter, Free Form Fibers, Saratoga Springs, NY

4:20-4:40pm T300HoneySiC - A New Near-Zero CTE CMC

W. Goodman, Trex Enterprises Corporation, Albuquerque, NM 4:40-5:00pm 3D Woven Carbon Composites for Weapons Components

Y. Chen, U.S. Army, RDECOM-ARDEC, Picatinny Arsenal, NJ 5:00-5:20pm A Solid Rocket Internal Insulation Ablation Mystery

C. Powars and C. Derbidge, St. Croix Research, San Jose, CA 5:20-5:40pm Phase Equilibria and Solidus Temperatures in the Re-Si-C, W-Si-C, Re-W-C and Re-Mo-C

Systems M. Opeka, D. Ramos and J. Zaykoski, Naval Surface Warfare Center, Carderock, West Bethesda, MD


THURSDAY MORNING – JANUARY 29, 2015 Session 1: Behavior and Life Ceramic Matrix Composites 3 Session Chairs: Craig Przybyla and Larry Zawada, Air Force Research Laboratory, Wright


Location: Salon 1 7:30-8:30am Registration and Continental Breakfast 8:15-8:20am Session Chairs Remarks 8:20-9:00am KEYNOTE: Matrix Cracking, Detection and Micromechanics of Pre-Preg Laminate SiC/SiC

Composites G. Morscher, N. Gordon and E. Maillet, University of Akron, Akron, OH

9:00-9:20am On the Necessity of Multi-Scale Damage Characterization in Ceramic Matrix Composites

S. Daly and J. Tracy, University of Michigan, Ann Arbor, MI 9:20-9:40am Developing New Test Methods for Ceramic Matrix Composites (CMC) Using Micro Digital Image

Correlation (DIC) E. Jones and G. Jefferson, Air Force Research Laboratory, Wright Patterson AFB, OH M. Braginsky, University of Dayton Research Institute, Dayton, OH B. Rooths, Southwest Ohio Council for Higher Education, Dayton, OH

9:40-10:00am Monitoring Damage Evolution in CMCs Using Acoustic Emission

T. Whitlow, Universal Technology Corporation, Dayton, OH E. Jones and C. Przybyla, Air Force Research Laboratory, Wright Patterson AFB, OH

10:00-10:20am BREAK 10:20-10:40am Test Methods and Prediction of Interlaminar Mode I and Mode II Fracture Toughness in Ceramic

Matrix Composites (CMC's) F. Abdi and C. Godines, AlphaSTAR Corporation, Long Beach, CA G. Morscher, University of Akron, Akron, OH J. Ahmad, Structural Analytics, Inc., Carlsbad, CA

10:40-11:00am Nondestructive Evaluation (NDE) for Behavior and Life Prediction of CMCs

E. Lindgren, Air Force Research Laboratory, Wright Patterson AFB, OH 11:00-11:20am Microstructural Characterization of Textile Architecture in SiC/SiC CMCs by Micro-CT

G. Jefferson, Air Force Research Laboratory, Wright Patterson AFB, OH T. Key and P. Mogilevsky, UES, Inc., Dayton, OH S. Safriet, University of Dayton Research Institute, Dayton, OH

11:20-11:40am Towards Virtual Testing of Ceramic Matrix Composites at the Constituent Length Scale

M. Czabaj, University of Utah, Salt Lake City, UT 11:40-12:00pm Quantitative NDE of CMCs by Microwave Interferometry

K. Schmidt and J. Little, Evisive, Inc., Baton Rouge, LA W. Ellingson, ERC Company, Indianapolis, IN


THURSDAY MORNING – JANUARY 29, 2015 Session 2: Hypersonic Materials 1 Session Chairs: Anthony Calomino, NASA Langley Research Center, Hampton, VA

Larry Hudson, NASA Dryden Research Center, Edwards, CA Location: Salon 2

7:30-8:30am Registration and Continental Breakfast 8:35-8:40am Session Chairs Remarks 8:40-9:00am Analysis of Alpha Silicon Carbide/Carbon Fibers for Use in Composites

J. Garnier, S. Perkins, K. Koller and M. Weseman, Advanced Ceramic Fibers, LLC, Idaho Falls, ID 9:00-9:20am Laser Bond Inspection of Composite Materials

D. Sokol, LSP Technologies, Dublin, OH 9:20-9:40am Development of Advanced C-C Composites for Missile TPS Applications

S. Violette, Fiber Materials Inc., Biddeford, ME 9:40-10:00am Continued Optimization of Low-Density Foam-Reinforced Ablatives for High-Velocity, High Heat

Flux Earth Return Missions S. Brown, B. Williams and V. Arrieta, Ultramet, Pacoima, CA B. Sullivan and M. Dion, Materials Research & Design, Inc., Wayne, PA M. Droege, Ocellus, Livermore, CA

10:00-10:20am BREAK 10:20-10:40am High-Rate Strain Testing of Aeroshell Material Employed on Space Nuclear Power Systems

D. Kramer, University of Dayton Research Institute, Dayton, OH


THURSDAY AFTERNOON – JANUARY 29, 2015 Session 1: Behavior and Life Ceramic Matrix Composites 4 Session Chairs: Craig Przybyla and Larry Zawada, Air Force Research Laboratory, Wright


Location: Salon 1 1:35-1:40pm Session Chairs Remarks 1:40-2:20pm KEYNOTE: Microstructure-sensitive Extreme Value Enviro-Mechanical Response

Characterization and Simulation in SiC/SiC Ceramic Matrix Composites C. Przybyla, J. Simmons, M. Uchic, E. Jones, R. Hay and L. Zawada, Air Force Research Laboratory, Wright Patterson AFB, OH S. Bricker and R. Hardie, University of Dayton, Dayton, OH R. Krishnamurthy, P. Mogilevsky and T. Parthasarathy, UES, Inc., Dayton, OH M. Braginsky and J. Pierce, University of Dayton Research Institute, Dayton, OH T. Whitlow, Universal Technology Corporation, Dayton, OH N. Engel, Southwest Ohio Council for Higher Education, Dayton, OH

2:20-2:40pm Multiscale Modeling of SiC/SiC Ceramic Matrix Composites

S. Mital, The University of Toledo, Toledo, OH S. Arnold, B. Bednarcyk and E. Pineda, NASA Glenn Research Center, Cleveland, OH

2:40-3:00pm Oxidation of Hi-Nicalon SiC Fibers

E. Opila and M. Wilson, University of Virginia, Charlottesville, VA 3:00-3:20pm BREAK 3:20-3:40pm Modeling Environmental Degradation of SiC-Fiber reinforced CMCs

T. Parthasarathy, UES, Inc., Dayton, OH C. Przybyla, R. Hay and M. Cinibulk, Air Force Research Laboratory, Wright Patterson AFB, OH

3:40-4:00pm The Role of Oxidation in Strain Accumulation for CMCs

Y. Gowayed and E. Abouzeida, Auburn University, Auburn, AL I. Smyth, Pratt & Whitney, East Hartford, CT G. Ojard, United Technologies Research Center, East Hartford, CT J. Ahmad and U. Santhosh, Structural Analytics, Inc., Carlsbad, CA G. Jefferson, Air Force Research Laboratory, Wright Patterson AFB, OH

4:00-4:20pm A Micromechanics-Based Model for Damage, Life and Residual Strength of Ceramic Matrix

Composite Structures in Oxidizing Environments U. Santhosh and J. Ahmad, Structural Analytics, Inc., Carlsbad, CA Y. Gowayed, Auburn University, Auburn, AL I. Symth, Pratt & Whitney, East Hartford, CT G. Ojard, United Technologies Research Center, East Hartford, CT G. Jefferson, Air Force Research Laboratory, Wright Patterson AFB, OH

4:20-4:40pm Surface Recession of Structural Ceramics in High-Temperature Flowing Steam Environments C. Barklay, S. Goodrich, L. Chuck and C. Sjöblom, University of Dayton Research Institute, Dayton, OH

4:40-5:00pm Ceramic Field Repair for Structurally Compliant, Dielectric Matched Component Restoration E. Pope, K. Ringled and S. Grandi, MATECH, Westlake Village, CA R. Batzer, Lockheed Martin Company, Dallas, TX M. O’Malley, Air Force Research Laboratory, Wright Patterson AFB, OH


THURSDAY AFTERNOON – JANUARY 29, 2015 Session 2: Hypersonic Materials 2 Session Chairs: Anthony Calomino, NASA Langley Research Center, Hampton, VA

Larry Hudson, NASA Dryden Research Center, Edwards, CA Location: Salon 2

Details coming soon…


Thank You to Our 2015 Sponsors!

Conference Program Chair

Dr. Mark M. Opeka Naval Surface Warfare Center, Carderock

Code 617 9500 MacArthur Boulevard

West Bethesda, MD 20817-5700 Phone: 301-277-3963

Email: [email protected]

mailto:[email protected]

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