|
PROGRAM
|
CUSTOMERS
|
YEAR
|
|
ATLAS Piece Part Processing
|
SGT, Inc. (ICESat-2/ATLAS-Instrument)
|
2009
|
|
Design and Fabriation of High Tempeature Large RTM Tool for Balistic Test
Panels
|
NASA Glenn / Clark Atlanta University HiPPAC Center
|
2009
|
|
Fabriction of Nano-Loaded Epoxy RTM PMC Panels
|
NASA Glenn / Clark Atlanta University HiPPAC Center
|
2009
|
|
Screening of High Temperature Resins
|
NASA Glenn / Clark Atlanta University HiPPAC Center
|
2009
|
|
RTM Test Panel Fabrication
|
Lockheed Martin Aero
|
2008
|
|
Nano-Particle Enhanced Polymer Materials for Space Flight Applications -
Phase II
|
NASA Goddard
|
2008
|
|
High Temperature Low Melt Viscosity Polyimides for Resin
Transfer Molding (RTM) –
|
AFOSR / NASA Glenn
|
2008
|
|
Development of In-Situ Grade IM7/MTM45-1 Tape and Fiber
Placement Efforts
|
Lockheed Martin Aero
|
2008
|
|
VARTM Processing of High Temperature Polymer Matrix
Composites
|
AFOSR /AFRL Phase I STTR
|
2007
|
|
Nano-Particle Enhanced Polymer Materials for Space Flight Applications -
Phase I
|
NASA Goddard
|
2007
|
|
Support Fabrication of In-Situ Grade IM7/M73 and Fiber
Placement Efforts
|
Lockheed Martin Aero
|
2007
|
|
In-Situ Fiber Placement Demonstration - Phase II
|
Lockheed Martin Aero
|
2007
|
|
Fabrication & Machining of Polymer Matrix Composite Test Panels
|
Lockheed Martin Aero
|
2007
|
|
Fabrication of Polymer Matrix Composite Test Article
|
Lockheed Martin Aero
|
2006
|
|
Thermal Panel Fabrication
|
Lockheed Martin Aero
|
2006
|
|
Fiber Metal Laminate Panel Fabrication
|
Lockheed Martin Aero
|
2006
|
|
In-Situ Fiber Placement Demonstration - Phase I
|
Lockheed Martin Aero
|
2006
|
|
Composite/Metallic
Structural Joining Concepts
|
USAF
SBIR Phase II
|
2006
|
|
Hybrid
Bonding
|
Lockheed
Martin Aero
|
2005
|
|
Biomedical
Hydrogels
|
Zimmer
Spine
|
2005
|
|
Polyimide
Adhesive Development
|
Advanced
Resonance Technologies Inc.
|
2005
|
|
PETI Post
Cure Optimization
|
UBE
America
|
2005
|
|
Low Cost
BMI
|
Lockheed
Martin Aero
|
2005
|
|
Composite/Metallic
Structural Joining Concepts
|
USAF
SBIR
|
2005
|
|
Crack
Propagation Testing
|
Lockheed
Martin Aero / CAI Program
|
2004
|
|
Failure
Initiation in Lap Shears
|
Lockheed
Martin Aero / CAI Program
|
2004
|
|
JSF High
Temp RTM
|
GDE LTD /
Rolls Royce
|
2004
|
|
RTM Fiber
and Binder Screening for F-35
|
Lockheed
Martin Aero
|
2004
|
|
PETI VARTM
|
LM-Denver
/ IRAD
|
2004
|
|
PETI
Property Development
|
UBE
America
|
2004
|
|
High Temp
RTM
|
Boeing
|
2003
|
|
RTM
Laminate Screening
|
Lockheed
Martin Aeronautics Co.
(Composites
Affordability Initiative)
|
2003
|
|
RTM
Mat’l Screening
|
Boeing
|
2003
|
|
Test and
Fab. of High Temperature RTM Composite Panels
|
NASA
Langley Research Center
|
2003
|
|
PETI-330
Evaluation
|
Raytheon /
UBE
|
2003
|
|
Resin
Screening & Property Dev.
|
Loctite
|
2003
|
|
RLV High
Temperature RTM
|
Northrop
Grumman
|
2003
|
|
JSF High
Temperature RTM
|
GDE LTD /
Rolls Royce
|
2003
|
|
High
Temperature RTM Tool Design and Fabrication
|
NASA Glenn
|
2003
|
|
RTM
Process Dev.
|
SRI / NASA
LaRC
|
2003
|
|
High
Temperature RTM of PETI's & BMI's
|
CAU / NASA
Langley / NASA Glenn
|
2002 -
2003
|
|
F/A-22 RTM
Resin Screening
|
Lockheed
Martin Aeronautics Co. / CAU
|
2002 -
2003
|
|
Carbon /
Carbon Composites In Improved Thermo-Oxidative Stability
|
USAF /
Triton Systems, Inc. / CAU
|
2002 -
2003
|
|
Comanche
In-Situ Fiber Placement Development
|
Lockheed
Martin Space Systems Co.
|
2002
|
|
P-3 Epoxy
VARTM
|
Lockheed
Martin Aeronautics Co.
|
2002
|
|
Nano-reinforced
Matrix for High Temperature Composites
|
Triton
Systems, Inc./NASA
|
2002
|
|
Thermoplastic
Blend, Optimization & Property Determination Study
|
CAU /
Lockheed Martin Aeronautics Co.
|
2002
|
M&P
Technologies, Inc.
