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Summary                               293


                     QUESTION 3: Suppose that we launch a body horizontally from the surface of the
                     Earth, with a velocity exactly equal to the escape velocity of 11.2 km/s. What kind of
                     orbit will this body have? Ignore atmospheric friction.
                     QUESTION 4: Uranus has a smaller gravitational acceleration at its surface than the
                     Earth. Can you conclude that the escape velocity from its surface is smaller than from
                     the Earth’s surface?
                     QUESTION 5: Suppose that three comets, I, II, and III, approach the Sun. At the
                     instant they cross the Earth’s orbit, comet I has a speed of 42 km/s, comet II has a
                     larger speed, and comet III a smaller speed. Given that the orbit of comet I is parabolic,
                     what are the kinds of orbit for comets II and III, respectively?
                        (A) Elliptical; hyperbolic (B) Elliptical; parabolic (C) Hyperbolic; elliptical
                        (D) Hyperbolic; parabolic (E) Parabolic; elliptical








                     SUMMARY



                     PHYSICS IN PRACTICE Communication Satellites                                                 (page 281)
                     and Weather Satellites

                     MATH HELP Ellipses                                                                           (page 283)

                     LAW OF UNIVERSAL GRAVITATION                                                                      (9.1)
                                                                        GMm                 The force on each
                     Magnitude:                                     F      2                particle is directed  m
                                                                          r                 toward the other
                                                                                            particle.
                     Direction: The force on each mass is directed
                                                                                                      r
                     toward the other mass.                                                    M
                                                                                        2
                     GRAVITATIONAL CONSTANT                         G   6.67   10  11  N m /kg 2                       (9.2)

                     ACCELERATION OF FREE FALL ON EARTH                 GM E                                           (9.6)
                                                                    g     2
                                                                         R E


                     SPEED FOR CIRCULAR ORBIT AROUND SUN                  GM                                          (9.10)
                                                                    v         S
                                                                        B r

                     PERIOD OF ORBIT AROUND SUN                           4p 2
                                                                      2
                                                                    T           r 3
                                                                         GM
                                                                             S
                     KEPLER’S FIRST LAW  The orbits of the planets are
                     ellipses with the Sun at one focus.

                     KEPLER’S SECOND LAW  The radial line segment                              S
                     from the Sun to a planet sweeps out equal areas in
                     equal times.                                                            Radial line sweeps out
                                                                                             equal areas in equal times.
                     KEPLER’S THIRD LAW  The square of the period is
                     proportional to the cube of the semimajor axis of a
                     planetary orbit.
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