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Cmh17 Mmc Cmc Properties: TRIMARC-1 Ti-6Al-2Sn-4Zr-2Mo wire fiber wound panel

73 1 Air 32.4 8·10-4 Fcy0.02 Mean to 73 1 Air 32.4 8·10-4 Fcy0.2 Minimum

CMH-17 Vol 4 Section 3 detailed statistical summary properties for metal matrix composites (MMC) and ceramic matrix composites (CMC). Includes fiber properties (Nextel 610, SCS-6), composite mechanical properties (Ftu, Fty, Fcy, Et, Ec, Poisson ratio, elongation) with full statistical data (mean, min, max, CV, B-value, distribution) across multiple temperatures and environments.

Aerospace Engineeringmaterial system: TRIMARC-1 Ti-6Al-2Sn-4Zr-2Mo wire fiber wound panel5 rowsPage 30 of 30
material systemcondition property statconditionorientation or layuppropertysource pagestatistictable idunitvaluevalue text
TRIMARC-1 Ti-6Al-2Sn-4Zr-2Mo wire fiber wound panel73 1 Air 32.4 8·10-4 Fcy0.02 Mean73 1 | Air | 32.4 | 8·10-4[0]Fcy0.02243Mean3.8.2.2.2(b)ksi185185
TRIMARC-1 Ti-6Al-2Sn-4Zr-2Mo wire fiber wound panel73 1 Air 32.4 8·10-4 Fcy0.02 Minimum73 1 | Air | 32.4 | 8·10-4[0]Fcy0.02243Minimum3.8.2.2.2(b)ksi11
TRIMARC-1 Ti-6Al-2Sn-4Zr-2Mo wire fiber wound panel73 1 Air 32.4 8·10-4 Fcy0.2 Maximum73 1 | Air | 32.4 | 8·10-4[0]Fcy0.2243Maximum3.8.2.2.2(b)ksi11
TRIMARC-1 Ti-6Al-2Sn-4Zr-2Mo wire fiber wound panel73 1 Air 32.4 8·10-4 Fcy0.2 Mean73 1 | Air | 32.4 | 8·10-4[0]Fcy0.2243Mean3.8.2.2.2(b)ksi329329
TRIMARC-1 Ti-6Al-2Sn-4Zr-2Mo wire fiber wound panel73 1 Air 32.4 8·10-4 Fcy0.2 Minimum73 1 | Air | 32.4 | 8·10-4[0]Fcy0.2243Minimum3.8.2.2.2(b)ksi11

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