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Chapter 13 Gravitation Newton’s law of gravitation • Any two (or more) massive bodies attract each other • Gravitational force (Newton's law of gravitation) m1m2 F G 2 rˆ r • Gravitational constant G = 6.67*10 –11 N*m2/kg2 = 6.67*10 –11 m3/(kg*s2) – universal constant Gravitation and the superposition principle • For a group of interacting particles, the net gravitational force on one of the particles is n F1,net F1i i2 • For a particle interacting with a continuous arrangement of masses (a massive finite object) the sum is replaced with an integral F1,body dF body Chapter 13 Problem 5 Three uniform spheres of mass 2.00 kg, 4.00 kg and 6.00 kg are placed at the corners of a right triangle. Calculate the resultant gravitational force on the 4.00-kg object, assuming the spheres are isolated from the rest of the Universe. Shell theorem • For a particle interacting with a uniform spherical shell of matter F1,shell dF shell • Result of integration: a uniform spherical shell of matter attracts a particle that is outside the shell as if all the shell's mass were concentrated at its center Gravity force near the surface of Earth • Earth can be though of as a nest of shells, one within another and each attracting a particle outside the Earth’s surface • Thus Earth behaves like a particle located at the center of Earth with a mass equal to that of Earth mEarthm1 ˆ GmEarth ˆ F1, Earth G 2 j 2 m1 j g m1 ˆj REarth REarth g = 9.8 m/s2 • This formula is derived for stationary Earth of ideal spherical shape and uniform density Gravity force near the surface of Earth In reality g is not a constant because: Earth is rotating, Earth is approximately an ellipsoid with a non-uniform density Gravitational field • A gravitational field exists at every point in space • When a particle is placed at a point where there is gravitational field, the particle experiences a force • The field exerts a force on the particle • The gravitational field is defined as: g Fg m • The gravitational field is the gravitational force experienced by a test particle placed at that point divided by the mass of the test particle Gravitational field • The presence of the test particle is not necessary for the field to exist • The source particle creates the field • The gravitational field vectors point in the direction of the acceleration a particle would experience if placed in that field GmEarth g 2 REarth • The magnitude is that of the freefall acceleration at that location Gravitational potential energy • Gravitation is a conservative force (work done by it is path-independent) • For conservative forces (Ch. 8): rf rf Gm1mEarth dr U F d r 2 r ri ri 1 1 Gm1mEarth r r f i Gravitational potential energy 1 1 U U f U i Gm1mEarth r r f i • To remove a particle from initial position to infinity 1 1 Gm1mEarth U U i Gm1mEarth ri ri • Assuming U∞ =0 Gm1mEarth U i (ri ) ri Gm1m2 U (r ) r Gravitational potential energy Gm1m2 U (r ) r Escape speed • Accounting for the shape of Earth, projectile motion (Ch. 4) has to be modified: 2 v ac g v gR R Escape speed • Escape speed: speed required for a particle to escape from the planet into infinity (and stop there) Ki U i K f U f 2 m1v Gm1m planet 00 2 R planet vescape 2Gm planet R planet Escape speed • If for some astronomical object vescape 2Gmobject Robject 3 10 m / s c 8 • Nothing (even light) can escape from the surface of this object – a black hole Chapter 13 Problem 30 (a) What is the minimum speed, relative to the Sun, necessary for a spacecraft to escape the solar system, if it starts at the Earth’s orbit? (b) Voyager 1 achieved a maximum speed of 125 000 km/h on its way to photograph Jupiter. Beyond what distance from the Sun is this speed sufficient to escape the solar system? Kepler’s laws Tycho Brahe/ Tyge Ottesen Brahe de Knudstrup (1546-1601) Johannes Kepler (1571-1630) Three Kepler’s laws • 1. The law of orbits: All planets move in elliptical orbits, with the Sun at one focus • 2. The law of areas: A line that connects the planet to the Sun sweeps out equal areas in the plane of the planet’s orbit in equal time intervals • 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 First Kepler’s law • Elliptical orbits of planets are described by a semimajor axis a and an eccentricity e • For most planets, the eccentricities are very small (Earth's e is 0.00167) Second Kepler’s law • For a star-planet system, the total angular momentum is constant (no external torques) L rp (r )(mv ) (r )( mr ) mr 2 const • For the elementary area swept by vector r 2 2 1 dA r d r dA (r )( rd ) 2 2 dt 2 dt dA L dt 2m Third Kepler’s law • For a circular orbit and the Newton’s Second law GMm GM 2 2 (m)( r ) 3 2 r r F ma • From the definition of a period T 2 T 2 4 2 2 4 3 T r GM 2 2 • For elliptic orbits 4 3 T a GM 2 2 Satellites • For a circular orbit and the Newton’s Second law 2 GMm v (m) F ma 2 r r • Kinetic energy of a satellite 2 GMm U mv K 2r 2 2 • Total mechanical energy of a satellite GMm GMm GMm E K U K 2r r 2r Satellites • For an elliptic orbit it can be shown GMm E 2a • Orbits with different e but the same a have the same total mechanical energy Chapter 13 Problem 26 At the Earth’s surface a projectile is launched straight up at a speed of 10.0 km/s. To what height will it rise? Ignore air resistance and the rotation of the Earth. Questions? Answers to the even-numbered problems Chapter 13 Problem 2 2.67 × 10−7 m/s2 Answers to the even-numbered problems Chapter 13 Problem 4 3.00 kg and 2.00 kg Answers to the even-numbered problems Chapter 13 Problem 10 (a) 7.61 cm/s2 (b) 363 s (c) 3.08 km (d) 28.9 m/s at 72.9° below the horizontal Answers to the even-numbered problems Chapter 13 Problem 24 (a) −4.77 × 109 J (b) 569 N down (c) 569 N up