1.

A 600 kg rocket is set for a vertical firing. If the exhaust speed is 1000 ms^(-1), the mass of the gas ejected per second to supply the thrust needed to overcome the weight of rocket is

Answer»

117.6 KG `s^(-1)`
58.6 kg `s^(-1)`
6 kg `s^(-1)`
76.4 kg `s^(-1)`

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