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P113 Gravitation: Lecture 3

P113 Gravitation: Lecture 3. Escape speed from orbit Planets and satellites: Keplers Laws Orbital energy. Escape from Earth’s Gravity.

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P113 Gravitation: Lecture 3

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  1. P113 Gravitation: Lecture 3 • Escape speed from orbit • Planets and satellites: Keplers Laws • Orbital energy 2006: Assoc. Prof. R. J. Reeves

  2. Escape from Earth’s Gravity • We know from everyday experience by throwing stones that they go higher up if we throw them with faster velocity. Can we derive an equation that will give the height as a function of velocity? • A mass m starts at the surface of the earth with vertical velocity v. It reaches an altitude h where it turns around and falls down. Conservation of energy gives: • Exercise: Complete the algebra to derive the following equation for h. 2006: Assoc. Prof. R. J. Reeves

  3. Escape from Earth’s Gravity - 2 • Solving for h gives 2006: Assoc. Prof. R. J. Reeves

  4. Escape from Earth’s Gravity - 3 • The negative altitude reached when the velocity was 100,000 m/s indicates the mass becomes unbound from the earth’s gravitational field. • The escape velocity from the earth’s surface is given by 2006: Assoc. Prof. R. J. Reeves

  5. Escape from Earth’s Gravity - 4 • Escape from earth requires 11.2 km/s = 40,000 km/hr! How do rockets manage this incredible speed? • 11.2 km/s is the required speed at the earth’s surface without any additional thrust being applied. • We could escape from earth at 40 km/hr providing we applied thrust greater than our weight all the way to the moon! • Rockets achieve a balance: • They start out less than 11.2 km/s but continue to apply thrust. • The necessary escape speed decreases as the altitude increases. • Eventually the rocket is travelling faster than the escape speed for its present altitude. The rocket motors can be turned off and then it’s glide to the moon! 2006: Assoc. Prof. R. J. Reeves

  6. Kepler’s Laws applied to the Planets - 1 • THE LAW OF ORBITS: All planets move in elliptical orbits with the Sun at one focus. • The orbit is characterised by its semimajor axisa and its eccentricitye. • Rp is the perihelion distance. • Ra is the aphelion distance. 2006: Assoc. Prof. R. J. Reeves

  7. Kepler’s Laws applied to the Planets - 2 2. THE LAW OF AREAS: A line that connects the planet to the Sun sweeps out equal areas in then plane of the planets orbit in equal time intervals. • Kepler’s second law is a statement of conservation of angular momentum. 2006: Assoc. Prof. R. J. Reeves

  8. Kepler’s Laws applied to the Planets - 3 3. THE LAW OF PERIODS: The square of the period of any planet is proportional to the cube of the semimajor axis of its orbit. 2006: Assoc. Prof. R. J. Reeves

  9. Solar system simulation • http://janus.astro.umd.edu/javadir/orbits/ssv.html 2006: Assoc. Prof. R. J. Reeves

  10. Orbital Energy - 1 • Kepler’s second law stipulates that the speed of a planet in orbit is faster when closer to the sun. Correspondingly, the gravitational potential energy is smaller (more negative) when closer. • Assume an exact circular orbit. Newton’s second law gives • The kinetic energy is then • The total energy of the orbit is 2006: Assoc. Prof. R. J. Reeves

  11. Orbital Energy - 2 • If the orbit is elliptical, the total energy is • The negative value for the total energy is a general indication of a bound system. • Question: Can you think of another bound system with a negative energy? 2006: Assoc. Prof. R. J. Reeves

  12. Problem 2006: Assoc. Prof. R. J. Reeves

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