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Problem:
A rocket is launched vertically upward. The rocket has a mass Mr and carries Mo of fuel. The fuel burns at a constant rate (ß) and leaves the rocket at speed Ve relative to the rocket. Assume constant gravity (9.8m/sec^2). There is an air resistance given by F(a) = -kV.
Where V is the velocity of the rocket.
Take:
k = .1 n-sec/m
ß = 100 kg/sec
Mr = 1000 kg
Mo = 10000 kg
Ve = 3000 m/sec
What is the terminal velocity of the rocket (the velocity when fuel runs out)?
-----
The general solution for this problem is an extension of conservation of momentum for a system of variable mass.
mdv/dt = ∑F(ext) + Vrel(dM/dt)
I have no problem when the external force is solely gravity, however, when this problem presents linear air resistance, I am running into a bit of trouble with the integration.
My setup of the differential equation is as follows:
Set dm/dt to constant. dM/dt = ß = 100 kg/sec.
(=)
mdv/dt = 100Ve - mg - kV
--->
dv/dt + kV/m = (100Ve/m - g)
I am attempting to integrate the velocity from V(0) to V(Terminal), and the time from t=0 to t=t(final)= Mo/ß = 10000/100 = 100 seconds.
My question is regarding the velocity portion of the differential equation.
I can't seem to get that V over to the left side of the integral by itself... and I'm wondering if I could get some sort of example on how to do that type of integration, or if I've gone astray somewhere.
Does this integration qualify as a first order differential?
i.e.
dy/dx + P(x)y = Q(x) ?
Addendum:
Okay, so I've set up the equation:
m/k(100Ve/m-g) - (m/k(100Ve/m-g)e^(-kt/m))
Thanks!
Sean
A rocket is launched vertically upward. The rocket has a mass Mr and carries Mo of fuel. The fuel burns at a constant rate (ß) and leaves the rocket at speed Ve relative to the rocket. Assume constant gravity (9.8m/sec^2). There is an air resistance given by F(a) = -kV.
Where V is the velocity of the rocket.
Take:
k = .1 n-sec/m
ß = 100 kg/sec
Mr = 1000 kg
Mo = 10000 kg
Ve = 3000 m/sec
What is the terminal velocity of the rocket (the velocity when fuel runs out)?
-----
The general solution for this problem is an extension of conservation of momentum for a system of variable mass.
mdv/dt = ∑F(ext) + Vrel(dM/dt)
I have no problem when the external force is solely gravity, however, when this problem presents linear air resistance, I am running into a bit of trouble with the integration.
My setup of the differential equation is as follows:
Set dm/dt to constant. dM/dt = ß = 100 kg/sec.
(=)
mdv/dt = 100Ve - mg - kV
--->
dv/dt + kV/m = (100Ve/m - g)
I am attempting to integrate the velocity from V(0) to V(Terminal), and the time from t=0 to t=t(final)= Mo/ß = 10000/100 = 100 seconds.
My question is regarding the velocity portion of the differential equation.
I can't seem to get that V over to the left side of the integral by itself... and I'm wondering if I could get some sort of example on how to do that type of integration, or if I've gone astray somewhere.
Does this integration qualify as a first order differential?
i.e.
dy/dx + P(x)y = Q(x) ?
Addendum:
Okay, so I've set up the equation:
m/k(100Ve/m-g) - (m/k(100Ve/m-g)e^(-kt/m))
Thanks!
Sean
Last edited: