NASA SBIR SUCCESS STORY   ARCHIVED - Data Not Current
 For Information Purposes Only



Glenn Research Center 
 
1994 Phase I - 1996 Phase II 

Non-Toxic, Resin Transfer Molding (RTM) Processable, High Temperature Matrix Resin 

Foster-Miller, Inc. 

Waltham, MA 
 

INNOVATION 
    RTM processable, high temperature (Tg>600°F), low toxicity matrix resin system
Composite Cylinders Manufactured via new RTM
Composite Cylinders Manufactured
via new RTM
Optional Powerpoint file
ACCOMPLISHMENTS 
    • Developed matrix resin system by combining reactive diluents with the NASA developed AMB-21 polyimide resin
    • Lowered the viscosity of the base resin significantly, decreased the amount of volatile by-products during cure, and increased cured Tg of AMB-21
    • Successfully fabricated demonstration composite cylinders by RTM
COMMERCIALIZATION 
    • Estimated market for RTM processable PMR-15 substitute is $20-40 M/year
    • Formed Pyrogonn l.l.c. for commercialization of this and related technologies
    • Sample materials provided to McDonnell-Douglas, Dow-UT NASA, and GE Engines, for testing and evaluation
     
GOVERNMENT/SCIENCE APPLICATIONS 
    • This resin system could replace PMR-15 as a high temperature organic matrix for carbon reinforced composites in aerospace propulsion systems and other high temperature structural applications where cost effective fabrication to near net-shape via RTM is desirable
     
For more information about this firm, please send e-mail to company representative 

Return to NASA SBIR Success Listings 

Curator: SBIR Support