This document specifies the conditions for determination of tensile properties of ceramic matrix composite
materials with continuous fibre reinforcement for temperatures up to 1 700 °C in air at atmospheric pressure.
This document applies to all ceramic matrix composites with a continuous fibre reinforcement, unidirectional
(1D), bi-directional (2D), and tri-directional (xD, with 2 < x <= 3), loaded along one principal axis of
reinforcement.
NOTE 1 In most cases, ceramic matrix composites to be used at high temperature in air are coated with an antioxidation
coating.
NOTE 2 The purpose of this document is to determine the tensile properties of a material when it is placed under an
oxidizing environment but not to measure material oxidation.
Dieses Dokument legt die Bedingungen zur Bestimmung der Eigenschaften von endlosfaserverstärkten keramischen Verbundwerkstoffen unter Zugbelastung bei Temperaturen bis zu 1 700 °C in Luft bei Atmosphärendruck fest.