Determine the nozzle throat area for a rocket engine producing a total – McqOptions

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1.	Determine the nozzle throat area for a rocket engine producing a total thrust of 10 kN, chamber pressure of 5.2 MPa and thrust coefficient of 1.9.
A.	10.12 cm<sup>2</sup>
B.	12.10 cm<sup>2</sup>
C.	11.20 cm<sup>2</sup>
D.	21.10 cm<sup>2</sup>
Answer» B. 12.10 cm<sup>2</sup>

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