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SPH4UI Gravitational Potential energy Mr. Burns Gravitational Potential Energy To explore how much energy a spacecraft needs to escape from Earth’s gravity, we must expand on the topic of gravitational potential energy. To calculate the change in gravitational potential energy that a mass undergoes when it undergoes a vertical displacement near the Earth’s surface, we used: UG mg h Where U G is the change in gravitational potential energy, m is the mass, g is the magnitude of the gravitational field constant, and h is the vertical displacement, where when we choose hi to be the ground, we simply obtain U=mgh. This equation assumes that g remains reasonably constant during the change in vertical displacement. We define the work done on a system by a specific conservative force as the negative of the change in a potential energy function associated with the force. Changes are always taken as final minus initial values Wconserv U f U i U Gravitational Potential Energy As we recall from the Kinetic energy Theorem: change in the Kinetic net work done on energy of a particle the particle EK EKf EKi W A force does positive work when it has a vector component in the same direction as the displacement. If the work done on a particle is positive, then the particles kinetic energy increases. Since the work done a we move a mass between two points is independent upon the path, the force is conservative Wconserv U EK Gravitational Potential Energy Change in potential energy is equal to the negative of the work done by the gravitational force on a mass U W W F x dx f Calculus definition of work i U F x dx f i U hf hi U mgh This gives us a Calculus definition of change in potential energy mg dh mgh f mghi Equation for change in potential energy If we set, hi to be zero (the ground), we obtain an simple formula to determine the potential energy Gravitational Potential Energy Work done by the gravitational force FG during the vertical motion of a mass from initial height y1 to final height y2 as the body rises. The gravitational potential energy U increases (negative work done by gravity, Kinetic Energy decreases). Work done by the gravitational force FG during the vertical motion of a mass from initial height y1 to final height y2 as the body rises. The gravitational potential energy U decreases (positive work done by gravity, Kinetic Energy increases) Gravitational Potential Energy But, how do we handle Gravitational Potential Energy, when g is not a constant (such as when we are not on Earth)? Gravitational Potential Energy Recall that the law of universal gravitation is given by: GMm FG 2 r Where FG is the magnitude of the force of gravitational attraction between any two objects, M is the mass of one object, m is the mass of the other object, and r is the distance between the centres of the two To increase the separation of the two masses requires work to be done. That is, we must do work to overcome the gravitational attraction between the two masses when moving mass m from distance r1 to distance r2 Work is done to overcome this distance r1 M m r2 Gravitational Potential Energy As the result of the work being done to increase the separation from r1 to r2, the gravitational potential energy of the system increases. The work done to change the separation from r1 to r2 is equal is equal to the change in gravitational energy from r1 to r2. However, recall that work done by a varying force is equal to the area under the force-displacement graph for that interval. Gravitational Potential Energy To find an expression for this work, we consider a body of mass m outside the Earth and compare the work Wgrav done by the gravitational force when a body moves directly away from or towards the centre of the Earth (from r=r1 to r=r2). r2 r2 r1 r1 Wgrav Fdr GmE m GmE m GmE m dr 2 r r2 r1 Because Force The path does not have to be a the straight line, it could also be a directly upon the initial and curve, but the work done points only depends toward the centre final values of r, not the path taken (this of is definition of a the Earth, F is conservative force). negative We now define the corresponding potential energy U so that Wgrav=U1-U2. Therefore we have a final definition of gravitational potential energy Gm1m2 U r Gravitational Potential Energy You may be troubled by the equation for gravitational potential energy because it states that it is always negative. But we have encountered this before, recall when we used U=mgh, we found that U could be negative whenever the body of mass was below the arbitrary height we chose h to be zero at. In using our equation, we have chosen U to be zero when the body of mass is infinitely far away from the Earth r . As the body moves towards the Earth, gravitational potential energy decreases and becomes negative. Gm1m2 U r Gravitational Potential Energy These formula seen initially confusing when first encountered. U mgh When gravity field is constant (near Earth) Gm1m2 U r Universal Potential energy, Equals zero when r approaches infinity But, they provide us with the same meaning. The change in gravitational energy at the Earth's Surface is just a special case of the general solution. This is the gravity well scientists talk about. Gravitational Potential Energy What is the change in gravitational potential energy of a 72.1 kg astronaut, lifted from Earth’s surface into a circular orbit at an altitude of 4.35 x 102 km? rE 6.38 106 m M E 5.98 1024 kg U U f U i GMm GMm r ri f 2 2 11 N m 24 11 N m 5.98 10 kg 72.1kg 6.67 10 5.98 1024 kg 72.1kg 6.67 10 2 2 kg kg 6 5 6 6.38 10 m 4.35 10 m 6.38 10 m 4.2198 109 J 4.5076 109 J 2.88 108 J Let’s approximate the answer using U=mgh U mgh Note: h is distance above the ground N 72.1kg 9.80 4.35 105 m kg 3.07 108 J Gravitational Potential Energy We can use the fact that if no other external forces besides gravity affect a mass, then the total energy is conserved (the gravitational force does work and thus the mechanical energy is conserved). The Kinetic Energy gained by the system is matched with the Potential Energy lost, and thus our mass will have the following statement of energy conservation.. EK 1 U1 EK 2 U 2 Now by inserting the formulas for the Kinetic and Potential Energy and interpreting the scenario where the object reaches the r location where both EK2 and U2 have a zero value (where the object comes to a stop). EK 1 U1 EK 2 U 2 EK 1 U1 0 1 2 GMm mvi 0 2 r 1 2 GMm mv 2 r 2GM v2 r 2GM v r This gives us the initial speed v1, needed for a body to escape from the surface of a spherical mass M with radius r This is the escape velocity of the mass Gravitational Potential Energy Suppose you want to place a 1000 kg weather satellite into a circular orbit 300 km above Earth’s surface. a) What speed, period, and radial acceleration must it have? b) How much work has to be done to place the satellite in orbit? c) How much additional work must be done to make this satellite escape Earth’s gravity ME=5.97x1024 kg RE=6380 km First we need the radius of the satellites orbit: r 6380km 300km 6680km 6.68 106 m Gravitational Potential Energy Suppose you want to place a 1000 kg weather satellite into a circular orbit 300 km above Earth’s surface. a) What speed, period, and radial acceleration must it have? b) How much work has to be done to place the satellite in orbit? c) How much additional work must be done to make this satellite escape Earth’s gravity For a stable orbit: FG=mac v2 GM E m m 2 r r v GM E r r 6.68 106 m 2 11 N m 5.97 1024 kg 6.67 10 2 kg v 6.68 106 m m 7720 s Gravitational Potential Energy Suppose you want to place a 1000 kg weather satellite into a circular orbit 300 km above Earth’s surface. a) What speed, period, and radial acceleration must it have? b) How much work has to be done to place the satellite in orbit? c) How much additional work must be done to make this satellite escape Earth’s gravity For a stable orbit: FG=mac 4 2 r GM E m r2 m 2 T 4 2 r 2 r T GM E 2 r v 2 6.68 106 m m 7720 s 5440 s 90.6 min r 6.68 106 m m v 7720 s Gravitational Potential Energy Suppose you want to place a 1000 kg weather satellite into a circular orbit 300 km above Earth’s surface. a) What speed, period, and radial acceleration must it have? b) How much work has to be done to place the satellite in orbit? c) How much additional work must be done to make this satellite escape Earth’s gravity r 6.68 106 m 2 v ac r 2 m 7720 s 6.68 106 m m 8.92 2 s m v 7720 s Gravitational Potential Energy b) How much work has to be done to place the satellite in orbit? The work required is the difference between the total mechanical energy when the satellite is in orbit (Ef) and when the satellite was on the launch pad (Ei). RE=6380 km R =6680 km ME=5.97x1024 kg W E f Ei EKf U f EKi U i E f EKf U f 1 GM E m GM E m mv 2 0 2 r r E 1 GM E m mv 2 2 r 2 2 11 N m 24 11 N m 24 2 6.67 10 5.97 10 kg 1000 kg 6.67 10 5.97 10 kg 1000 kg 2 1 1 GM GM 2 2 m m kg kg E E 1000kg 7720 m 6 6 r r 10 m s 6.68 10 m 6.38 2 2 GM E m circular orbit 2r 2.99 1010 J 6.25 1010 J 3.26 1010 J Gravitational Potential Energy c) How much additional work must be done to make this satellite escape Earth’s gravity • We recall that for a satellite to escape to infinity, the total mechanical energy must be zero. • The total mechanical energy in orbit Ef was -2.99 x 1010 J • To increase this to zero, an amount of work equal to 2.99 x 1010 J must be done. Gravitational Potential Energy A 5.00x102 kg weather satellite is to be placed into a circular geosynchronous orbit (one orbit is 24 hours) around Earth . M E 5.98 1024 kg rE 6.38 106 m a) What is the radius of the satellite’s orbit? b) What is the velocity of the satellites orbit? c) What is the gravitational potential energy (universal) of the satellite when it is at rest on Earth’s surface? d) What is the total energy of the satellite when it is in geosynchronous orbit? e) How much work the launch rocket do on the satellite to place it into orbit? f) Once in orbit, how much additional energy would the satellite require to escape from Earth’s potential well? g) What should the launch velocity be it the satellite is required to escape from Earth’s potential well? Gravitational Potential Energy A 5.00x102 kg weather satellite is to be placed into a circular geosynchronous orbit (one orbit is 24 hours) around Earth . M E 5.98 1024 kg rE 6.38 106 m a) What is the radius of the satellite’s orbit? Fc FG GM E mS r2 GM ac 2 E r mS ac 4 2 r GM E 2 T2 r GM ET 2 r 4 2 3 GM ET 2 r 4 2 3 Since we are given the period of the orbit is 24 hours. We will use the Period version of centripetal acceleration. 2 2 11 N m 24 6.67 10 5.98 10 kg 24 h 3600 s 3 kg 2 4 2 4.23 107 m Gravitational Potential Energy A 5.00x102 kg weather satellite is to be placed into a circular geosynchronous orbit (one orbit is 24 hours) around Earth . M E 5.98 1024 kg rE 6.38 106 m b) What is the velocity of the satellites orbit? v GM E r 2 11 N m 5.98 1024 kg 6.67 10 2 kg 4.23 107 m 3070 m s 1.11104 km h Gravitational Potential Energy A 5.00x102 kg weather satellite is to be placed into a circular geosynchronous orbit (one orbit is 24 hours) around Earth . M E 5.98 1024 kg rE 6.38 106 m c) What is the gravitational potential energy (universal) of the satellite when it is at rest on Earth’s surface? UG GM E ms rE 2 N m 11 24 2 6.67 10 5.98 10 kg 5.00 10 kg 2 kg 6.38 106 m 3.13 1010 J Gravitational Potential Energy A 5.00x102 kg weather satellite is to be placed into a circular geosynchronous orbit (one orbit is 24 hours) around Earth . M E 5.98 1024 kg rE 6.38 106 m d) What is the total energy of the satellite when it is in geosynchronous orbit? ET K U 1 2 GM E ms mv 2 r 1 GM E ms 2 r 2.36 109 J Gravitational Potential Energy A 5.00x102 kg weather satellite is to be placed into a circular geosynchronous orbit (one orbit is 24 hours) around Earth . M E 5.98 1024 kg rE 6.38 106 m e) How much work does the launch rocket do on the satellite to place it into orbit? W E E f Ei 2.36 109 J 3.13 1010 J 2.89 1010 J Gravitational Potential Energy A 5.00x102 kg weather satellite is to be placed into a circular geosynchronous orbit (one orbit is 24 hours) around Earth . M E 5.98 1024 kg rE 6.38 106 m f) Once in orbit, how much additional energy would the satellite require to escape from Earth’s potential well? The negative of Total Energy to get the satellite there. 2.36 10 J 9 Gravitational Potential Energy A 5.00x102 kg weather satellite is to be placed into a circular geosynchronous orbit (one orbit is 24 hours) around Earth . M E 5.98 1024 kg rE 6.38 106 m g) What should the launch velocity be if the satellite is required to escape from Earth’s potential well? vE 2GM E rE 2 11 N m 24 5.98 10 kg 2 6.67 10 2 kg 6.38 106 m 4 m 1.12 10 s Gravitational Potential Energy Suppose your hand moves up 0.50m while you are throwing a ball ( 0.145kg), which leaves your hand with an upward velocity of 20.0 m/s. Assuming your hand exerts a constant upward force on the ball, determine the magnitude of this force. Determine the speed of the ball 15.0 m above the point where it leaves your hand. We will look at the energy diagrams for y1, y2, and y3 to guide us in solving this problem Gravitational Potential Energy Suppose your hand moves up 0.50m while you are throwing a ball (0.145kg), which leaves your hand with an upward velocity of 20.0 m/s. Assuming your hand exerts a constant upward force on the ball, determine the magnitude of this force. Determine the speed of the ball 15.0 m above the point where it leaves your hand. The ball’s motion has two stages: while it is in contact with your hand and after it leaves your hand To keep track of these stages, we let point 1 be where your hand first starts to move, and point 2 where the ball leaves your hand, and point 3 where the ball is 15.0m above point 2. 3 2 1 Gravitational Potential Energy Suppose your hand moves up 0.50m while you are throwing a ball (0.145kg), which leaves your hand with an upward velocity of 20.0 m/s. Assuming your hand exerts a constant upward force on the ball, determine the magnitude of this force. Determine the speed of the ball 15.0 m above the point where it leaves your hand. The non gravitational force of your hand acts only between points 1 and 2. using a coordinate system with point 2 being at 0m K 1 U1 Whand and point 3 at 15.0m E and point 1 at -0.50m,1 provides mv12 mgy1 Whand us with a easy application 2 of conservative energies to m 0 J solve kg problem. 0.145this 9.80 2 0.50m Whand s Whand The kinetic energy increases by 29.0J and the potential energy increases by 0.71J, the change in total mechanical energy 29,7J is due to the work by your hand. 3 EK 2 U 2 1 2 mv2 mgy2 2 2 2 1 m m 0.145kg 20.0 0.145kg 9.8 2 0.0m 2 s s EK 2 EK 1 U 2 U1 29.0 J 0 J1 0 0.71J 29.7 J Gravitational Potential Energy Suppose your hand moves up 0.50m while you are throwing a ball (0.145kg), which leaves your hand with an upward velocity of 20.0 m/s. Assuming your hand exerts a constant upward force on the ball, determine the magnitude of this force. Determine the speed of the ball 15.0 m above the point where it leaves your hand. Since the force done by your hand was a constant force,, the Whand done by this force is equal to the force multiplied by the upward displacement (y2-y1) Whand F y2 y1 F 3 2 Whand y2 y1 29.7 J 0.50m 59 N 1 Gravitational Potential Energy Suppose your hand moves up 0.50m while you are throwing a ball (0.145kg), which leaves your hand with an upward velocity of 20.0 m/s. Assuming your hand exerts a constant upward force on the ball, determine the magnitude of this force. Determine the speed of the ball 15.0 m above the point where it leaves your hand. EK 2 U 2To Efind U 3 speed at point K 3 the EK 33, we EK 2 note U 2 that U 3 the total 3 energy 1 2mechanical 1 2 mv3between mv2 points mgy2 mgy 3 2 and 3 2 2 are conserved, Therefore we can use: 2 EK2+U m 2=EmK3+U3 v3 v22 2 g y2 y3 20.0 2 9.8 2 0m 15m s s m 10.3 s 2 1