Calculate the temperature coefficient

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Reference no: EM131401212

What is the ratio of the burning area to the nozzle throat area for a solid propellant motor with these characteristics? Also, calculate the temperature coefficient

(a) and the temperature sensitivity of pressure (π_K).

Reference no: EM131401212

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Calculate the temperature coefficient : What is the ratio of the burning area to the nozzle throat area for a solid propellant motor with these characteristics? Also, calculate the temperature coefficient (a) and the temperature sensitivity of pressure (πK).

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