A rocket of mass 6000kg is fired from earth ,so that exhaust speed of gas is 1 km/s . The rate of ejection of gas ,so that the rocket lift with initial acceleration of 20 m/s^2 is
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Dear Student,
◆ Answer -
dm/dt = 180 kg/s
◆ Explanation -
For the rocket to move with acceleration a, thrust required is -
F = m(a+g) ...(1)
To provide this thrust, let dm/dt be rate of ejection of gas.
F = v(dm/dt) ...(2)
From (1) & (2),
m(a+g) = v(dm/dt)
dm/dt = m(a+g)/v
dm/dt = 6000 × (20+10)/1000
dm/dt = 180 kg/s
Therefore, rate of ejection of gas should be 180 kg/s.
Thanks dear...
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