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please answer Question 1 (a) Describe the main components of rocket engine and its functions. [3 mark] (h) Use the concept of linear impulse and

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Question 1 (a) Describe the main components of rocket engine and its functions. [3 mark] (h) Use the concept of linear impulse and Figure 0.1 to derive the thrust equation. [3 mark] (b) time (I-d1 Figure (11 (c) Under what nozzle conditions is a rocket motor said to be optimized (Le. produces maximum thrust), use a diagram to explain your reasoning. [2 marks]

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