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Question 1: What challenges arise in "Real-Time System Testing" for aerospace applications, and how do you ensure that systems perform as expected under real-world conditions?

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Question 2: When conducting vibration testing on a new aerospace prototype, what is the goal of the test?

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Question 3: How can you ensure the long-term reliability of a spacecraft's electronic systems in a harsh space environment?

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Question 4: What is the purpose of using finite element analysis (FEA) in system testing?

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Question 5: What is the primary advantage of using "Composite Materials" in aerospace applications, and what are the challenges in their use?

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Question 6: How does "Integrated Testing" improve system performance validation in aerospace, particularly when multiple subsystems are involved?

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