A rocket of mass 120 kg is fired in the gravity free space. It ejects gases with velocity 600 m/s at the rate of 1 kg/s, what is the initial thrust on the rocket ?
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Answered by
26
Here,
M = 120 kg
u = 600 m/s
dm/dt = -1 kg/s
negative because mass is decreasing with time
From Rocket propulsion analysis we have
mdv = -udm
=> dv/dm = -u/m ---1.
We know from Momentum equation
Let m be the mass of the rocket at an instant and v its velocity at instant
F = d/dt(mv)
= v(dm/dt) + m(dv/dt)
Using chain rule
dv/dt = (dv/dm)(dm/dt)
F = v(dm/dt) + m(dv/dm)(dm/dt)
Using eqn. 1
= v(dm/dt) + m(-u/m)(dm/dt)
= v(1) – u(-1)
= v + u
At the beginning velocity of the rocket was 0,
v = 0
F = u = 600
So initial thrust = 600 N
Initial acceleration = 600/120 = 5 ms-2
M = 120 kg
u = 600 m/s
dm/dt = -1 kg/s
negative because mass is decreasing with time
From Rocket propulsion analysis we have
mdv = -udm
=> dv/dm = -u/m ---1.
We know from Momentum equation
Let m be the mass of the rocket at an instant and v its velocity at instant
F = d/dt(mv)
= v(dm/dt) + m(dv/dt)
Using chain rule
dv/dt = (dv/dm)(dm/dt)
F = v(dm/dt) + m(dv/dm)(dm/dt)
Using eqn. 1
= v(dm/dt) + m(-u/m)(dm/dt)
= v(1) – u(-1)
= v + u
At the beginning velocity of the rocket was 0,
v = 0
F = u = 600
So initial thrust = 600 N
Initial acceleration = 600/120 = 5 ms-2
Answered by
3
M=120kg, v=600m/s
A=5m/s^2
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