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A 5000 kg rocket is set for vertical firing. The exhaust speed is 800 ms–1. To give an initial upward acceleration of 20 ms–2, the amount of gas ejected per second to supply the needed thrust will be (g = 10 ms–2) 

(1) 127.5 kg s–1

(2) 187.5 kg s–1

(3) 185.5 kg s–1

(4) 137.5 kg s–1

PMT