A rocket of mass 1000 Kg set for vertical firing the exhaust speed is 200 m/s to give on initial acceleration of what will be the amount of gas ejected per second (in Kg/s ) to supply the needed thrust (g = 10 m/s )
125
100
150
75
As we have learned
Acceleration of Rocket -
- wherein
Instantaneous Velocity of Rocket
Force applied by the gases on the rocket =
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