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Question 1: How does "thermal management" play a critical role in the design and testing of aircraft prototypes?

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Question 2: How does the certification process address the role of aircraft systems (such as avionics and landing gear) in overall airworthiness?

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Question 3: What is the primary challenge when testing an aircraft's control response during a steep climb?

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Question 4: In prototype aircraft design, what is the role of structural testing at various load factors (e.g., ultimate, limit, and proof loads)?

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Question 5: When conducting a takeoff performance test, what is the primary variable to measure?

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Question 6: When designing a flight test program, what is the most important factor to ensure comprehensive coverage of aircraft performance?

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