Find the height if an orbiting satellite given only velocity.

Click For Summary
SUMMARY

The discussion focuses on calculating the height of an orbiting satellite given its velocity, specifically for a satellite at 2 Mm above Earth's surface. The key equations used include the modified gravitational acceleration formula, g' = g * (R_earth^2 / R_orbit^2), and the centripetal acceleration formula, a = v^2 / R_orbit. The conclusion emphasizes that it is unnecessary to calculate g' directly; instead, one can derive the orbital radius and velocity using the relationship between gravitational force and centripetal acceleration.

PREREQUISITES
  • Understanding of circular motion and centripetal acceleration
  • Familiarity with gravitational force equations
  • Knowledge of basic algebra and symbolic manipulation
  • Concept of orbital mechanics and satellite dynamics
NEXT STEPS
  • Study the derivation of gravitational force and centripetal acceleration equations
  • Learn about orbital mechanics and the significance of orbital radius
  • Explore the concept of symbolic problem-solving in physics
  • Investigate the effects of altitude on gravitational acceleration
USEFUL FOR

Students in physics, aerospace engineers, and anyone interested in satellite dynamics and orbital mechanics will benefit from this discussion.

lubo
Messages
35
Reaction score
0

Homework Statement



An Earth satellite is to be put into orbit at a height of 2 Mm above the Earth's surface. Determine the velocity it must have. Make the following assumptions: (a) the orbit is circular; (b) the Earth is a sphere of radius 6•37 Mm; (c) gravity decreases as an inverse square law.


(MY main question is to get an idea of how to find the height above the Earth's surface of the satellite, when you are only given the Velocity of a satellite in orbit).

Homework Equations



g' (acceleration due to gravity at a distance R to the centre of the earth)=g*r earth^2/R orbit^2

a=V^2/r orbit



The Attempt at a Solution



g'=?
g=9.81
r earth=6.37Mm
R orbit=6.37 + 2(height)

g' = 9.81*6.37^2/(2+6.37^2)
g'=5.682m/s^2

a=v^2/R therefore v^2=8.37*10^6 * 5.682 Therefore V=6896 m/s

However if I try to work back using V only V=6896 m/s and find the height 2Mm, I can only use g=9.81. Therefore I cannot find g' to allow me to find Ro (re + h). Then I could take Ro from re and I would have the height.

i.e. a=v^2/R = 6896^2/r Earth as I don't have R orbit = 6896^2/6.37*10^6 = 7.465m/s^2

If I try g' =mg then I do not have a mass.

If I try a=rw^2 and find w then I can only use re and a=9.81. Therefore I cannot find the g'= 5.682m/s^2

If I substitute g' with rw^2 and get Ro^3=g*r^2/w^2 I am still only using r of Earth and w from r and not a time period or R orbit

I hope all this makes sense, Thanks for any help.
 
Physics news on Phys.org
lubo said:

The Attempt at a Solution



g'=?
g=9.81
r earth=6.37Mm
R orbit=6.37 + 2(height)

g' = 9.81*6.37^2/(2+6.37^2)
g'=5.682m/s^2

a=v^2/R therefore v^2=8.37*10^6 * 5.682 Therefore V=6896 m/s

However if I try to work back using V only V=6896 m/s and find the height 2Mm, I can only use g=9.81. Therefore I cannot find g' to allow me to find Ro (re + h). Then I could take Ro from re and I would have the height.

i.e. a=v^2/R = 6896^2/r Earth as I don't have R orbit = 6896^2/6.37*10^6 = 7.465m/s^2

So what you did is that you found the value for g at the distance Rorbit, then used g =v2/Rorbit to get v. Then used v to get back Rorbit ?

If you need to get the velocity, why are you getting the height above the Earth's surface for?

Though if you needed to get 'h' using v you would just use

GMm/(R+h)2 = mv2/(R+h)

mass of satellite m cancels out, M and G are constants and so is R.
 
lubo said:
However if I try to work back using V only V=6896 m/s and find the height 2Mm, I can only use g=9.81. Therefore I cannot find g' to allow me to find Ro (re + h). Then I could take Ro from re and I would have the height.

i.e. a=v^2/R = 6896^2/r Earth as I don't have R orbit = 6896^2/6.37*10^6 = 7.465m/s^2
You can't arbitrarily use Rearth just because you don't have Rorbit.
If I try g' =mg then I do not have a mass.
This doesn't make sense at all. You have an acceleration on the lefthand side and a force on the righthand side of the equation. They can't be equal.
If I try a=rw^2 and find w then I can only use re and a=9.81. Therefore I cannot find the g'= 5.682m/s^2

If I substitute g' with rw^2 and get Ro^3=g*r^2/w^2 I am still only using r of Earth and w from r and not a time period or R orbit

I hope all this makes sense, Thanks for any help.
The problem is you're trying to find a number for an intermediate result, g', that you don't have enough information to find. You don't need to calculate the number, though.

The way you solved the problem initially was saying the acceleration due to gravity the satellite experiences is[tex]g' = g\frac{R_\mathrm{Earth}^2}{R_\mathrm{orbit}^2}[/tex]This acceleration is also the centripetal acceleration needed for the circular orbit, so you have
[tex]g' = \frac{v^2}{R_\mathrm{orbit}}[/tex]
Now if you had combined these two equations, you would have gotten
[tex]g\frac{R_\mathrm{Earth}^2}{R_\mathrm{orbit}^2} = \frac{v^2}{R_\mathrm{orbit}}[/tex]
If, as in this problem, you're given Rorbit, you can solve for the speed v. On the other hand, if you were given v instead, you could solve the equation for Rorbit. In either case, you don't need to calculate the value of g'.

Avoiding the stumbling block you encountered is one of the reasons why your instructor has likely encouraged you to work out problems symbolically and to plug numbers in only near the end. I really encourage you to get into this habit. It'll save you a lot of headaches down the road.
 

Similar threads

  • · Replies 16 ·
Replies
16
Views
3K
  • · Replies 6 ·
Replies
6
Views
3K
Replies
5
Views
3K
  • · Replies 15 ·
Replies
15
Views
2K
Replies
5
Views
3K
  • · Replies 39 ·
2
Replies
39
Views
4K
  • · Replies 63 ·
3
Replies
63
Views
5K
Replies
1
Views
2K
Replies
2
Views
4K
Replies
38
Views
4K