1.

A rocket whose initial mass is 850 kg consumes fuel at the rate of 2.3 kgs-1, The speed of the exhaust gases relative to the rocket engine is 2000 ms-1. What thrust does the rocket engine provide?

A. 5.47 x 106 N
B. 4600 N
C. 1217 N
D. 6440 N
Answer» C. 1217 N


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