Second Kepler law for hyperbolas

In summary, a body can have three types of orbits around another body: an ellipse, a hyperbola, or a parabola. The second law of Kepler, also known as the area law, applies to all types of central force motion, including hyperbolic and parabolic orbits. This can be proven using the fact that the angular momentum of the particle remains constant and the area swept out by the particle in a given time interval is proportional to its rate of change.
  • #1
jaumzaum
434
33
A body can describe 3 types of orbits around another (considering only the gravitational force), a elipse, a hyperbole or a parabola.
Does the second kepler law (area law) work for hyperboles or parabolas too?
 
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  • #2
Yes. Kepler's 2nd law holds for any central force motion. Here is one proof:

Consider a particle moving under a central force ##F = f(r)\hat{r}##. We see immediately that ##\frac{\mathrm{d} L}{\mathrm{d} t} = r\times F = 0## hence ##L = r\times p## is a constant of motion. Now consider the position of the particle at an instant ##t## and another instant ##t + \Delta t## so that the position of the particle is given in polar coordinates by ##(r,\theta)## and ##(r + \Delta r, \theta + \Delta \theta)## respectively. For small ##\Delta \theta##, the area swept out during this interval will be given by the triangle swept out of side length ##r + \Delta r## and height ##r\Delta \theta## so ##\Delta A = \frac{1}{2}r^{2}\Delta \theta + \frac{1}{2}r\Delta r \Delta \theta ## hence ##\frac{\Delta A}{\Delta t} = \frac{1}{2}r^{2}\frac{\Delta \theta}{\Delta t} + \frac{1}{2}r\frac{\Delta r \Delta \theta }{\Delta t}## so ##\frac{dA}{dt} = \lim_{\Delta t\rightarrow 0 }\frac{\Delta A}{\Delta t} = \frac{1}{2}r^{2}\frac{d\theta}{d t} = \text{const.} ## as desired.
 
  • #3
Spelling error. You are talking about hyperbolas. Hyperbole is a completely different thing.
 

Related to Second Kepler law for hyperbolas

What is the Second Kepler law for hyperbolas?

The Second Kepler law for hyperbolas states that the line connecting a planet to the sun sweeps out equal areas in equal time intervals. This law applies to planets that follow a hyperbolic orbit around the sun.

How is the Second Kepler law for hyperbolas different from the Second Kepler law for ellipses?

The Second Kepler law for hyperbolas is different from the Second Kepler law for ellipses because it applies to planets that have a hyperbolic orbit, while the Second Kepler law for ellipses applies to planets with an elliptical orbit. This means that the shape of the planet's orbit determines which law applies.

What is the significance of the Second Kepler law for hyperbolas?

The Second Kepler law for hyperbolas helps scientists understand the motion of planets in a hyperbolic orbit around the sun. It also allows scientists to make predictions about the position of the planet at a given time, based on the amount of area it has swept out in a certain amount of time.

What factors affect the application of the Second Kepler law for hyperbolas?

The Second Kepler law for hyperbolas is affected by the eccentricity of the planet's orbit and the mass of the sun. A higher eccentricity or a more massive sun will result in a faster sweeping of areas, while a lower eccentricity or a less massive sun will result in a slower sweeping of areas.

How is the Second Kepler law for hyperbolas used in real-world applications?

The Second Kepler law for hyperbolas is used in astrodynamics to calculate the trajectories of spacecraft and other objects in hyperbolic orbits. It is also used in studying comets and other celestial bodies that follow hyperbolic orbits around the sun.

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