- #1
kalupahana
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1. Problem
A launched rocket emitting gas with a speed of 1500 m/sec relative to rocket and with flowrate of 100 kg/sec.
If net mass of rocket is 5000 kg, find it's acceleration.
2. Equations
F=ma
F=d(mv)/dt
Conservation of momentum
m1u1 + m2u2 = m1v1 + m2v2
3.Attempt
Flowrate = 100 kg/s
velocity = 1500 m/s
momentum downwards = mv = 100 x 1500 = 1.5 x 105 kg m/s
According to conservation of momentum, i found the velocity to upward direction.
m1u1 + m2u2 = m1v1 + m2v2
0 = -100 x 1500 + 5000v2
5v2 = 150
v2 = 30 m/s
what should do next to find the acceleration
If I use F=d(mv)/dt
what is the initial velocity and final velocity. I have no idea about those two & and how to take it.
A launched rocket emitting gas with a speed of 1500 m/sec relative to rocket and with flowrate of 100 kg/sec.
If net mass of rocket is 5000 kg, find it's acceleration.
2. Equations
F=ma
F=d(mv)/dt
Conservation of momentum
m1u1 + m2u2 = m1v1 + m2v2
3.Attempt
Flowrate = 100 kg/s
velocity = 1500 m/s
momentum downwards = mv = 100 x 1500 = 1.5 x 105 kg m/s
According to conservation of momentum, i found the velocity to upward direction.
m1u1 + m2u2 = m1v1 + m2v2
0 = -100 x 1500 + 5000v2
5v2 = 150
v2 = 30 m/s
what should do next to find the acceleration
If I use F=d(mv)/dt
what is the initial velocity and final velocity. I have no idea about those two & and how to take it.