1.

A 600 kg rocket is set for a vertical firing. If the exhaust speed is \[1000\text{ }m{{s}^{-1}}\], the mass of the gas ejected per second to supply the thrust needed to overcome the weight of rocket is

A. \[117.6\text{ kg}{{\text{s}}^{-1}}\]
B. \[58.6\text{ kg}{{\text{s}}^{-1}}\]
C. \[6\text{ kg}{{\text{s}}^{-1}}\] 
D. \[76.4\text{ kg}{{\text{s}}^{-1}}\]
Answer» D. \[76.4\text{ kg}{{\text{s}}^{-1}}\]


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