Effects of preform structure on mechanical properties of carbon-carbon composite for nozzle exit cone

Xiao Hu Zhang, He Jun Li, Zhi Biao Hao, Hong Cui, A. Lin Ji

Research output: Contribution to journalArticlepeer-review

1 Scopus citations

Abstract

Three types of carbon fiber reinforced preforms such as carbon cloth ply perform (P preform), needled caborn cloth preform (N preform) and braided carbon fiber perform (B preform) were designed to prepare carbon-carbon exit cone of nozzle, and the effects of the preform structures on the mechanical properties of carbon-carbon composite were compared and investigated. The results show that for same density C/C exit cone composite, interlaminar shear strength (ILSS) of C/C composite prepared by P preform has the lowest value, but ILSS of C/C composite prepared by N preform reaches the highest value. The high-temperature bending properties of C/C composite prepared by three types of preforms are almost the same, and N preform structure is more appropriate for preparation and forming of C/C exit cone composite.

Original languageEnglish
Pages (from-to)380-383
Number of pages4
JournalGuti Huojian Jishu/Journal of Solid Rocket Technology
Volume29
Issue number5
StatePublished - Oct 2006

Keywords

  • Carbon-carbon composites
  • Mechanical properties
  • Nozzle exit cone
  • Preform structure

Fingerprint

Dive into the research topics of 'Effects of preform structure on mechanical properties of carbon-carbon composite for nozzle exit cone'. Together they form a unique fingerprint.

Cite this