QCAA Aerospace Systems Practice Questions - QCAA Aerospace Systems External Assessment (Queensland) Exam

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What is the primary advantage of Carbon Fiber Reinforced Polymer (CFRP) over conventional aluminum alloys in modern aircraft construction?

Higher strength-to-weight ratio and superior fatigue resistance Lower material purchasing cost and easier visual crack inspection High electrical conductivity preventing lightning strike damage without protection Isotropic material properties in all loading directions without directional laying

Correct Answer:

Higher strength-to-weight ratio and superior fatigue resistance

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