Determine the chamber pressure for a rocket engine if the thrust coeff – McqOptions

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1.	Determine the chamber pressure for a rocket engine if the thrust coefficient is 1.8, the throat area is 0.2 m² and the total thrust is 20000 N.
A.	61.33 kPa
B.	67.98 kPa
C.	45.67 kPa
D.	55.56 kPa
Answer» E.

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