A 6000 - kg rocket is set for firing . If the exhaust speed is `1000 ms^(-1)` , how much gas must be ejected per second to supply the thrust needed , (a) to overcome the weight of the rocket , (b) to give the rocket an initial acceleration of `19.6 ms^(-2)`?

A rocket is set for vertical firing If the exhaust speed is 1200ms^(-1) , how much gas must be ejected per second to supply the thrust needed (i) to overcome the weight of rocket (ii) to give to the rocket an initial vertical upward acceleration of 29.6 m//s^(2) Given mass of rocket = 6000 kg.

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

A 600 kg rocket is set for vertical firing. If the exhaust speed is 1000m/s, the mass of the gas ejected per second to supply the thrust needed to overcome the weight of rocket is

A 600 kg rocket is set for a vertical fliring. If the exhaust speed is 100 m//s , the mass of the gas ejected per second to supply the thrust needed to overcome the weight of rocket is

A 600 Kg, rocket is set for a vertical firing. If the exhaust speed is 1000 m//s , the gas ejected per sec. to supply the thrust needed to overcome the weight of rocket is ...