Impression Creep of PMR-15 Resin at Elevated Temperatures

Abstract

The polyimides formed from the polymerization of monomeric-reactants (PMR) approach have been increasingly used as matrix materials in fiber-reinforced composites on aerospace and space structures for high temperature applications. The performance of PMR-based structures depends on the mechanical durability of PMR resins at elevated temperatures, including creep and stress relaxation. In this work, the creep behavior of PMR-15 resin was studied using the impression technique in the temperature range of 76-381 MPa. It was found that there existed a steady state creep for the creep tests performed at temperatures of 563 K and higher, from which a constant impression velocity was calculated. The steady state impression velocity increased with temperature and punching stress with the stress exponent in the range of 1.5-2.2. The average of the apparent activation energy of the PMR-15 was calculated at 122.7 +/- 6.1 kJ/mol.

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Document Details

Document Type
Technical Report
Publication Date
Jan 01, 2010
Accession Number
ADA513403

Entities

People

  • Fuqian Yang
  • G. A. Schoeppner
  • G. P. Tandon
  • Rong Chen
  • Yili Lu

Organizations

  • University of Kentucky

Tags

Communities of Interest

  • Space

DTIC Thesaurus Topics

  • Abstracts
  • Composite Materials
  • Copyrights
  • Creep
  • Creep Tests
  • Engineering
  • Fiber Reinforced Composites
  • Heat Of Activation
  • High Temperature
  • Information Operations
  • Materials
  • Materials Engineering
  • Materials Science
  • Polymers
  • Steady State

Fields of Study

  • Materials science

Readers

  • Combustion science or combustion engineering.
  • Polymer Science and Engineering.
  • Structural Health Monitoring of Composite Structures.

Technology Areas

  • Space