Search NASA⌕ Search

NASA NTRS · 19890043203

Toughening of a thermoplastic matrix composite - Processing issues

Abstract

The use of a rubber modified thermoplastic resin has been investigated as a method to improve the impact damage and the Mode I interlaminar fracture toughness of a unidirectional continuous carbon fiber composite. Test results show that the improvement in the fracture toughness is less than expected due to rubber particle agglomeration, poor fiber/matrix adhesion and the induced crystallization of the matrix. These restrictions must be eliminated in order to evaluate the maximum potential of a rubber toughened thermoplastic matrix on a composite's fracture toughness.

Keep this discovery

Explore connections, maps & timelines

BibTeXRIS

Parker, D. S., Yee, A. F.. 1988-01-01. Toughening of a thermoplastic matrix composite - Processing issues. https://ntrs.nasa.gov/citations/19890043203

Cite the original work for its findings. Save a collection to share your selection of sources.