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Celestial Mechanics Physics 201 Lecture 10

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Physics 201 Lecture 10. Celestial Mechanics. Newton’s triumph was to derive Kepler’s three laws of planetary motion. Kepler’s three laws: The orbit of every planet is an ellipse with the Sun at one of the foci - PowerPoint PPT Presentation

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Page 1: Celestial Mechanics

Celestial Mechanics

Physics 201 Lecture 10

Page 2: Celestial Mechanics

• Kepler’s three laws:– The orbit of every planet is an ellipse

with the Sun at one of the foci – A line joining a planet and the Sun

sweeps out equal areas during equal intervals of time

– The square of the orbital period is proportional to the cube of the orbital size

• Newton showed how these laws all follow from

Newton’s triumph was to derive Kepler’s three laws of planetary motion

Page 3: Celestial Mechanics

Everything you must know about ellipses – and nothing more

Orbitalparameters

Geometricparameters

Eccentricity

Orbital period

Page 4: Celestial Mechanics

Polar components of kinetic energy lead to the “effective potential”

Kinetic energy

“Effective potential”

Page 5: Celestial Mechanics

Using the effective potential makes this a one-dimensional problem

The trajectory of the particle does not depend on its mass – to make things a bit simpler, both energy and angular momentum will be implicitly divided by mass.

Page 6: Celestial Mechanics

Planning a trip in space? Manage your Δv budget

The Hohmann transfer orbitLongest time of transitMinimum Δv budget

“Get to low-Earth orbit, and you’re halfway to anywhere in the solar system” – Robert A. Heinlein

Page 7: Celestial Mechanics

Gravitational slingshot can be a huge source of Δv – e.g., Cassini probe to Saturn

Venus 1 Flyby Venus 2

Flyby

EarthFlyby

TargetingManeuver

JupiterFlyby

Page 8: Celestial Mechanics

Escape velocity and unbound orbits

• Adding speed increases energy and makes the orbit more linear

• If total energy is positive, the orbit will not return

• Five probes will escape our solar system…

No return

Escape orbit

Elliptical orbit

Circular orbit

Semi-latus rectum

  Launch date

Distance (AU)

Speed (AU/yr)

Working?

Pioneer 10 Mar 1972 107 2.54 no

Pioneer 11 Apr 1973 86.8 2.40 no

Voyager 2 Aug 1977 100 3.26 yes

Voyager 1 Sep 1977 122 3.60 yesNew

Horizons Jan 2006 24.8 3.21 yes