Conceptual Physics Projectiles Motion of Planets

Size: px

Start display at page:

Download "Conceptual Physics Projectiles Motion of Planets"

Mark Mason
5 years ago
Views:

1 Conceptual Physics Projectiles Motion of Planets Lana Sheridan De Anza College July 13, 2015

2 Last time angular momentum gravity gravitational field black holes

3 Overview projectile motion orbital motion Kepler s Laws escape speed

4 from Equations 4.3 and 4.6, which give Motion in 2 directions Imagine S v 5 d an rs 5air dx hockey puck moving with horizontally constant dt dt i^ 1 dy dt j^ 5 v x i^ 1 v y j^ (4.7) velocity: vectors, y elocity, in ure, s that nsions two ns in ctions. a b y x x Figure across a table at directio in the y puck, th ponent ponent in the p If it experiences a momentary upward (in the diagram) acceleration, it will have a component of velocity upwards. The horizontal motion remains unchanged! 1 Figure from Serway & Jewett, 9th ed.

5 nts Motion of Vectors in 2 directions can be resolved into horizontal and Motion in perpendicular directions can be analyzed separately. ents. A vertical force (gravity) does not affect horizontal motion. The horizontal component of velocity is constant. 1 Drawing by Hewitt, via Pearson.

6 Projectiles projectile Any object that is thrown. We will use this word specifically to refer to thrown objects that experience a vertical acceleration g.

7 Projectiles projectile Any object that is thrown. We will use this word specifically to refer to thrown objects that experience a vertical acceleration g. For projectile motion, we assume air resistance is negligible. This gives symmetrical parabolic trajectories. Why do we care?

8 Projectiles projectile Any object that is thrown. We will use this word specifically to refer to thrown objects that experience a vertical acceleration g. For projectile motion, we assume air resistance is negligible. This gives symmetrical parabolic trajectories. Why do we care?

9 Projectiles projectile Any object that is thrown. We will use this word specifically to refer to thrown objects that experience a vertical acceleration g. For projectile motion, we assume air resistance is negligible. This gives symmetrical parabolic trajectories. Why do we care?

10 Projectile Velocity 4 v y i y The y component of velocity is zero at the peak of the path. S vi u i v xi v y u S v v xi v y 0 S v The projectile is launched S with initial velocity v i. v y S g v xi u S v v y The x component of velocity remains constant because there is no acceleration in the x direction. v xi u i S v x Section 4.2, we stated that two-dimensional motion with constant accele 1 Figure from Serway & Jewett, 9th ed.

11 Projectile Velocity 4 v y i y The y component of velocity is zero at the peak of the path. S vi u i v xi v y u S v v xi v y 0 The projectile is launched S with initial velocity v i. But the y acceleration is not zero! S v v y S g v xi u S v v y The x component of velocity remains constant because there is no acceleration in the x direction. v xi u i S v x Section 4.2, we stated that two-dimensional motion with constant accele 1 Figure from Serway & Jewett, 9th ed.

12 Motion of projectiles We already considered the motion of objects dropped from rest at time t = 0, allowed to fall freely. (Calling down positive.) Velocity of the object at time t: v = v i + gt Distance the object falls in time t: d = 1 2 gt2

13 Acceleration due to gravity and kinematics nts of Vectors Let s think about the components of the motion separately. can be resolved into horizontal and ents. Vertical (y-direction): v y = v i,y gt d y = v i,y t 1 2 gt2 Horizontal (x-direction): a x = 0, v x = v i,x d x = v i,x t 1 Drawing by Hewitt, via Pearson.

14 Projectile s Trajectory erand y d in a y 5 two tion O y S vit S rf 1 t 2 2 gs (x,y) x Figure 4.8 The position vector The object would move in a straight line, but the force of gravity causes it S to fall as it moves to the right. r f of a projectile launched from the origin whose initial velocity 1 Figure from Serway & Jewett, 9th ed.

15 volve an algebraic argument. Motion in 2 Dimensions A method of testing that the vectors add as asserted! y Target Cengage Learning/Charles D. Winters Gun 0 u i Line of sight x T Point of collision 1 2 gt 2 x T tan u i y T x b tiflash photograph 1 Figure fromof Serway the projectile target & Jewett, 9th ed. demonstration. If the gun

16 Example Problem Suppose the pellet-gun on the previous slide can fire the pellet with an extremely high velocity. (a) How many meters below the line of sight would the pellet be after 5 seconds? (b) If the horizontal component of the pellet s velocity is 20 m/s, how far downrange is the pellet after those 5 seconds? 0 See Hewitt, page 175.

17 Example Problem Suppose the pellet-gun on the previous slide can fire the pellet with an extremely high velocity. (a) How many meters below the line of sight would the pellet be after 5 seconds? (b) If the horizontal component of the pellet s velocity is 20 m/s, how far downrange is the pellet after those 5 seconds? (Hint: we can consider each component of the velocity separately.) 0 See Hewitt, page 175.

18 Another example, problem 1, page 192 A ball is thrown horizontally from a cliff at a speed of 10 m/s. What will its speed be (roughly) after 1s? 0 See Hewitt, page 192.

19 Last one, # 4, page 192 A steel ball is fired horizontally at 8.0 m/s from from a 1.0 m-high table top. Show that a 20 cm tall coffee can placed on the floor 3.2 m from the base of the table will catch the ball.

20 Last one, # 4, page 192 A steel ball is fired horizontally at 8.0 m/s from from a 1.0 m-high table top. Show that a 20 cm tall coffee can placed on the floor 3.2 m from the base of the table will catch the ball. for a falling object d = 1 2 at2

21 uiz Effect 4.3 Rank of changing the launch launch angles for angle the five paths in Figure 4.10 w t to time of flight from the shortest time of flight to the longest. y (m) v i 50 m/s Complementary values of the initial angle u i result in the same value of R x (m) 1 Figure from Serway & Jewett, 9th ed.

Satellites Imagine now that you could throw an object straight out horizontally so fast that as it falls it matches the Earth s curvature. The object falls 1 m in 0.45 s.

22 Satellites Imagine now that you could throw an object straight out horizontally so fast that as it falls it matches the Earth s curvature. The object falls 1 m in 0.45 s. If it goes forward 3,570 m in that time, then the Earth s surface has also curved one meter away over that distance. This corresponds to a speed of 7, 900 m/s. 1 Figure from College Physics, OpenStax College, Ch 3, pg 110.

23 Satellites This is the same principle by which the Moon stays in orbit around the Earth. The Moon is the Earth s natural satellite. The same idea is applied to artificial satellites that are put into orbit around the Earth. The are moving at very high speeds and continuously falling around the Earth. Satellites can have many purposes, eg. telecommunications weather and Earth-monitoring GPS (global positioning system) human spaceflight and experiments

24 Some Types of Earth-Orbit Low Earth Orbit (LEO) - altitude from 160 km to 2,000 km with a period of minutes; all human spaceflight except Apollo has been in this orbit (or suborbital), also Earth observation satellites

25 Some Types of Earth-Orbit Low Earth Orbit (LEO) - altitude from 160 km to 2,000 km with a period of minutes; all human spaceflight except Apollo has been in this orbit (or suborbital), also Earth observation satellites Medium Earth Orbit (MEO) - altitude from 2,000 km to 35,786 km; GPS satellites

26 Some Types of Earth-Orbit Low Earth Orbit (LEO) - altitude from 160 km to 2,000 km with a period of minutes; all human spaceflight except Apollo has been in this orbit (or suborbital), also Earth observation satellites Medium Earth Orbit (MEO) - altitude from 2,000 km to 35,786 km; GPS satellites Polar Sun synchronous orbit - a particular set of low-to-medium Earth orbit that moves through passes through the equator at the same local time on each pass; orbital photography satellites

27 Some Types of Earth-Orbit Low Earth Orbit (LEO) - altitude from 160 km to 2,000 km with a period of minutes; all human spaceflight except Apollo has been in this orbit (or suborbital), also Earth observation satellites Medium Earth Orbit (MEO) - altitude from 2,000 km to 35,786 km; GPS satellites Polar Sun synchronous orbit - a particular set of low-to-medium Earth orbit that moves through passes through the equator at the same local time on each pass; orbital photography satellites Geosynchronous Orbit (GSO) - altitude of 35,786 km, the orbiting object orbits the Earth in one day - if it is in an equatorial orbit (GEO), it stays above a fixed point on the Earth s surface and appears fixed in the sky; telecommunications satellites

28 Satellites Imagine now that you could throw an object straight out horizontally so fast that as it falls it matches the Earth s curvature. The object falls 1 m in 0.45 s. If it goes forward 3,570 m in that time, then the Earth s surface has also curved one meter away over that distance. This corresponds to a speed of 7, 900 m/s.

29 Satellites This is the same principle by which the Moon stays in orbit around the Earth. The Moon is the Earth s natural satellite. The same idea is applied to artificial satellites that are put into orbit around the Earth. The are moving at very high speeds and continuously falling around the Earth. Satellites can have many purposes, eg. telecommunications weather and Earth-monitoring GPS (global positioning system) human spaceflight and experiments

30 Some Types of Earth-Orbit Low Earth Orbit (LEO) - altitude from 160 km to 2,000 km with a period of minutes; all human spaceflight except Apollo has been in this orbit (or suborbital), also Earth observation satellites

31 Some Types of Earth-Orbit Low Earth Orbit (LEO) - altitude from 160 km to 2,000 km with a period of minutes; all human spaceflight except Apollo has been in this orbit (or suborbital), also Earth observation satellites Medium Earth Orbit (MEO) - altitude from 2,000 km to 35,786 km; GPS satellites

32 Some Types of Earth-Orbit Low Earth Orbit (LEO) - altitude from 160 km to 2,000 km with a period of minutes; all human spaceflight except Apollo has been in this orbit (or suborbital), also Earth observation satellites Medium Earth Orbit (MEO) - altitude from 2,000 km to 35,786 km; GPS satellites Polar Sun synchronous orbit - a particular set of low-to-medium Earth orbit that moves through passes through the equator at the same local time on each pass; orbital photography satellites

33 Some Types of Earth-Orbit Low Earth Orbit (LEO) - altitude from 160 km to 2,000 km with a period of minutes; all human spaceflight except Apollo has been in this orbit (or suborbital), also Earth observation satellites Medium Earth Orbit (MEO) - altitude from 2,000 km to 35,786 km; GPS satellites Polar Sun synchronous orbit - a particular set of low-to-medium Earth orbit that moves through passes through the equator at the same local time on each pass; orbital photography satellites Geosynchronous Orbit (GSO) - altitude of 35,786 km, the orbiting object orbits the Earth in one day - if it is in an equatorial orbit (GEO), it stays above a fixed point on the Earth s surface and appears fixed in the sky; telecommunications satellites

34 Motion of the Planets The planets in our solar system orbit the Sun. (As planets in other systems orbit their stars.) This is called a heliocentric model.

35 Motion of the Planets The planets in our solar system orbit the Sun. (As planets in other systems orbit their stars.) This is called a heliocentric model. Nicolaus Copernicus (early 1500s A.D.) is credited with the paradigm since he developed a mathematical model and took seriously the idea that the implication was that the Earth moved around the Sun, but others had similar thoughts: Aristarchus of Samos (c. 270 BCE) Martianus Capella (400s A.D.) Aryabhata (500s A.D.), Nilakantha Somayaji (1500s A.D.) Najm al-dīn al-qazwīnī al-kātibī (1200s A.D.)

36 Motion of the Planets After Copernicus s proposal, Tycho Brahe gathered a lot of data about the positions of stars and planets. Johannes Kepler inherited Brahe s data and did the calculations to deduce a complete model. Galileo gathered additional data that supported the heliocentric model and popularized it.

37 Kepler s Laws Kepler s Three laws give simple rules for predicting stable planetary orbits. 1. All planets move in elliptical orbits with the Sun at one focus. 2. The a line from the Sun to a planet sweeps out equal areas of space in equal time intervals. 3. The square of the orbital period of any planet is proportional to the cube of the distance from the planet to the Sun. (T 2 r 3 )

38 is Kepler s the semicenter of the First Law: axis has Elliptical length b. Orbits Defining an ellipse: un, the Sun y the general re zero. The ection com-, c increases correspond or an ellipse length a, and the semiminor r 1 r 2 F 1 c a F 2 b x eccentricity er hand, the Figure 13.6a cury s orbit. rom a circle, a is the semimajor Each axis focus is located a 2 at = a b 2 + c 2 b is the semiminordistance axis c from the center. c is the distance from the center of the ellipse to the focus e is the eccentricity of the ellipse e = c/a Figure 13.5 Plot of an ellipse.

39 Kepler s First Law: Elliptical Orbits All planets move in elliptical orbits with the Sun at one focus. er 13 Universal Gravitation pe of h has ) the e of the shape comet ger The Sun is located at a focus of the ellipse. There is nothing physical located at the center (the black dot) or the other focus (the blue dot). Sun Orbit of Comet Halley Sun Center Orbit of Mercury Comet Halley Center a b The planets orbits are close to circular. (Mercury s is the between the planet and the Sun is a 1 c. At this point, called the aphelion, the planet is at its maximum distance from the Sun. (For an object in orbit around the least circular.) Earth, this point is called the apogee.) Conversely, when the planet is at the right end of the Halley s ellipse, the Comet distance hasbetween an orbit the planet with and a high the Sun eccentricity. is a 2 c. At this point, called the perihelion (for an Earth orbit, the perigee), the planet is at its minimum distance from the Sun. Kepler s first law is a direct result of the inverse-square nature of the gravita-

40 tional force. Circular M p and elliptical the gravitational force center. Thes K that move repeatedly S around S the S Sun F are also unbound objects, g v a such as el The radius vector drawn from the the SunMSun to S a once planetand sweeps then out never return to equal areas in equal time intervals. these objects also varies as the inve ta allowed paths for these objects inclu What does it mean? ra a th Kepler s Second Law: Equal Areas in Equal Time M p Kepler s Second Law Kepler s second S law can d S r be S v dt shown a S S r Sun F g v angular Sun momentum. Consider a p elliptical orbit (Fig. 13.7a). Let s con M S to be so much more da massive than th tational force exerted by the Sun Eo radius vector, directed toward the S a this central force about an S axis thro The area swept out by r in When the planet is closer to the Sun, it Therefore, must be moving because faster. the external a time interval dt is half the S d S r S v dt an isolated area of system the parallelogram. for angular mom va r Sun planet is a constant of the motion: th S K

41 Kepler s Third Law: T 2 r 3 The square of the orbital period of any planet is proportional to the cube of the distance from the planet to the Sun. T 2 = K s r 3 where K s is a constant, K s = 4π2 GM s = s 2 m 3.

42 Escape Speed escape speed The speed an object would need to have at Earth surface to have enough kinetic energy to leave Earth, overcoming the attraction of Earth s gravity. The object will convert its kinetic energy to potential energy as it moves higher and higher, away from the Earth.

43 Escape Speed which is the energy equivalent of 89 gal of gasoline. NASA engi craft as it ejects burned fuel, something we have not done her effect of this changing mass to yield a greater or a lesser amoun How fast does an object need to be projected with to escape Earth s gravity? Escape Speed R E S v f S v i m 0 h r max Suppose an object of mass m i with an initial speed v i as illust to find the value of the initial tance away from the center of system for any configuration. the Earth, v 5 v i and r 5 r i 5 R v f 5 0 and r 5 r f 5 r max. Beca these values into the isolated- Solving for v i 2 gives 1 2 M E Figure An object of mass m projected upward from For a given maximum altitud required initial speed. We are now in a position t speed the object must have a

44 Escape Speed To escape the surface of the Earth, an object must have a starting speed of v e = m/s = 11.2 km/s For other planets / celestial bodies the escape speeds can also be defined. The escape speed depends on the radius of the body and its mass. For the Sun, the escape speed at its surface is much higher: v e = 620 km/s

45 Summary projectile motion orbits motion of planets and satellites Kepler s laws escape speed Homework Hewitt, Ch 10, onward from page 190. Exercises: 15, 19, 23, 45, 59; Problems: 3 Study! read through the textbook

Conceptual Physics Projectiles Motion of Planets

Conceptual Physics Projectiles Motion of Planets Lana Sheridan De Anza College July 19, 2017 Last time angular momentum gravity gravitational field black holes Overview projectile motion orbital motion