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Question 1: In testing aerospace systems, what is the primary advantage of using hardware-in-the-loop (HIL) simulations?

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Question 2: How does the "Technology Readiness Level" (TRL) framework apply to the technology transfer process in aerospace, and how do you determine the readiness for transfer?

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Question 3: In prototype development, what is the primary benefit of using computer-aided design (CAD) software?

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Question 4: In prototype development for aerospace systems, which of the following is the most critical factor when choosing materials?

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Question 5: What is the primary advantage of using superalloys in turbine engines for aerospace applications?

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Question 6: What is the role of failure analysis in the technology transfer process?

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