- #1
Rapier
- 87
- 0
Problem:
In analogy to the Bohr Theory of the hydrogen atom, develop a quantum theory of Earth satellites, obtaining expressions for the orbit radius (r) and the energy (E) in terms of the quantum number (n) and the other relevant parameters. A satellite of mass 1000 kg is in a circular orbit of radius 7000 km, to what value of n does this correspond?
Equations and Constants:
Bohr Model: E = -R*h/n^2
E = 1/2 * m * r^2 * ω*2
ω = v/r
v^2 = G*M/r
R = 1.0973 x 10^7 m^-1
h = 6.626x10^34 kg*m^2/s
M = 5.972x10^24 kg
G = 6.674x10^-11 m^3/(kg*s^2)
Attempt:
E = -R*h/n^2
1/2 * m * r^2 * ω*2 = -Rh/n^2
r^2 = -2*R*h/(n^2 * ω^2 * m)
r^2 = -2*R*h*r^3/(n^2 * G* M * m)
1/r = -2*R*h/(n^2 * G* M * m)
r = (n^2 * G* M * m) / (-2*R*h)
Just by parsing the units I know I've taken a wrong turn. I've tried multiple times and I appear to be missing a velocity term somewhere with the (-2*R*h). I think I'm missing something simple, I just don't see it.
Thanks.
In analogy to the Bohr Theory of the hydrogen atom, develop a quantum theory of Earth satellites, obtaining expressions for the orbit radius (r) and the energy (E) in terms of the quantum number (n) and the other relevant parameters. A satellite of mass 1000 kg is in a circular orbit of radius 7000 km, to what value of n does this correspond?
Equations and Constants:
Bohr Model: E = -R*h/n^2
E = 1/2 * m * r^2 * ω*2
ω = v/r
v^2 = G*M/r
R = 1.0973 x 10^7 m^-1
h = 6.626x10^34 kg*m^2/s
M = 5.972x10^24 kg
G = 6.674x10^-11 m^3/(kg*s^2)
Attempt:
E = -R*h/n^2
1/2 * m * r^2 * ω*2 = -Rh/n^2
r^2 = -2*R*h/(n^2 * ω^2 * m)
r^2 = -2*R*h*r^3/(n^2 * G* M * m)
1/r = -2*R*h/(n^2 * G* M * m)
r = (n^2 * G* M * m) / (-2*R*h)
Just by parsing the units I know I've taken a wrong turn. I've tried multiple times and I appear to be missing a velocity term somewhere with the (-2*R*h). I think I'm missing something simple, I just don't see it.
Thanks.