Our Our Place Place in in the the Cosmos Cosmos
Lecture 8 Non-Circular Orbits and Tides
Non-Circular Orbits
- In the previous lecture we saw that Newton’s
universal law of gravitation Fg = G x m1 x m2 / r2 can explain Kepler’s laws of planetary motion in the special case of circular orbits
- A full mathematical derivation of elliptical
- rbits is beyond the scope of this course
- We can, however, gain some intuitive
understanding of non-circular orbits
Non-Circular Orbits
- Consider a satellite in a circular orbit and
imagine giving a boost to its orbital velocity
- Earth’s gravitational pull is unchanged but the
greater speed of the satellite causes it to climb above a circular orbit and hence its distance from Earth (“vertical distance”) increases
- Exactly like a ball thrown in the air, the pull
- f gravity slows vertical motion until vertical
motion stops and is then reversed as ball/satellite falls back towards Earth, gaining speed on the way Captions
Non-Circular Orbits
- The further a satellite pulls away from the
Earth, the more slowly it moves, until it reaches a maximum distance
- It then falls back towards the Earth, gaining
speed as it does so
- This is true for any object on an elliptical
- rbit about a more massive body, including a
planet orbiting the Sun
- Gravity thus explains Kepler’s 2nd law, why
planets sweep out equal areas in equal times
Escape Velocity
- Gravity also predicts unbound orbits
- The greater the speed of a satellite at closest
approach, the further it is able to pull away from the Earth and the more eccentric its orbit
- If a satellite is is moving faster than its escape
velocity gravity is unable to reverse its outward motion
- The satellite then coasts away from Earth, never to
return
- One can show that the escape velocity is a factor 2
larger than the circular velocity vesc = [2G M/r] = 2 vcirc - about 11 km/s on Earth