NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Process Optimization of Bismaleimide (BMI) Resin Infused Carbon Fiber CompositeBismaleimide (BMI) resins are an attractive new addition to world-wide composite applications. This type of thermosetting polyimide provides several unique characteristics such as excellent physical property retention at elevated temperatures and in wet environments, constant electrical properties over a vast array of temperature settings, and nonflammability properties as well. This makes BMI a popular choice in advance composites and electronics applications [I]. Bismaleimide-2 (BMI-2) resin was used to infuse intermediate modulus 7 (IM7) based carbon fiber. Two panel configurations consisting of 4 plies with [+45deg, 90deg]2 and [0deg]4 orientations were fabricated. For tensile testing, a [90deg]4 configuration was tested by rotating the [0deg]4 configirration to lie orthogonal with the load direction of the test fixture. Curing of the BMI-2/IM7 system utilized an optimal infusion process which focused on the integration of the manufacturer-recommended ramp rates,. hold times, and cure temperatures. Completion of the cure cycle for the BMI-2/IM7 composite yielded a product with multiple surface voids determined through visual and metallographic observation. Although the curing cycle was the same for the three panellayups, the surface voids that remained within the material post-cure were different in abundance, shape, and size. For tensile testing, the [0deg]4 layup had a 19.9% and 21.7% greater average tensile strain performance compared to the [90deg]4 and [+45deg, 90deg, 90deg,-45degg] layups, respectively, at failure. For tensile stress performance, the [0deg]4 layup had a 5.8% and 34.0% greater average performance% than the [90deg]4 and [+45deg, 90deg, 90deg,-45deg] layups.
Document ID
20130011578
Acquisition Source
Kennedy Space Center
Document Type
Conference Paper
Authors
Ehrlich, Joshua W.
(NASA Kennedy Space Center Cocoa Beach, FL, United States)
Tate, LaNetra C.
(NASA Kennedy Space Center Cocoa Beach, FL, United States)
Cox, Sarah B.
(NASA Kennedy Space Center Cocoa Beach, FL, United States)
Taylor, Brian J.
(NASA Kennedy Space Center Cocoa Beach, FL, United States)
Wright, M. Clara
(NASA Kennedy Space Center Cocoa Beach, FL, United States)
Caraccio, Anne J.
(NASA Kennedy Space Center Cocoa Beach, FL, United States)
Sampson, Jeffery W.
(NASA Kennedy Space Center Cocoa Beach, FL, United States)
Date Acquired
August 27, 2013
Publication Date
January 1, 2013
Subject Category
Composite Materials
Report/Patent Number
KSC-2013-013
KSC-2013-013R
Meeting Information
Meeting: Society for the Advancement of Materials and Process Engineering (SAMPE) 2013
Location: Long Beach, CA
Country: United States
Start Date: May 6, 2013
End Date: May 9, 2013
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available