Two Earth satellites, A and B, each of mass m, are to be launched into circular...

Two Earth satellites, A and B, each of mass m, are to be launched into circular orbits about Earth's center. Satellite A is to orbit at an altitude of 6660 km. Satellite B is to orbit at an altitude of 23200 km. The radius of Earth R_Eis 6370 km. (a) What is the ratio of the potential energy of satellite B to that of satellite A, in orbit? (b) What is the ratio of the kinetic energy of satellite B to that of satellite A, in orbit? (c)Which satellite (answer A or B) has the greater total energy if each has a mass of 17.0 kg? (d) By how much?

Answers to 3 significant digits and please show unit of measurement

Solutions

Expert Solution

Please rate me by giving me a like or thumb because it motivates me to do more work.

Thank you.

genius_generous answered 2 months ago

Next > < Previous

Related Solutions

Two Earth satellites, A and B, each of mass m, are to be launched into circular...

Two Earth satellites, A and B, each of mass m, are to be launched into circular orbits about Earth's center. Satellite A is to orbit at an altitude of 6820 km. Satellite B is to orbit at an altitude of 18100 km. The radius of Earth REis 6370 km. (a) What is the ratio of the potential energy of satellite B to that of satellite A, in orbit? (b) What is the ratio of the kinetic energy of satellite B...

Two Earth satellites, A and B, each of mass mmm = 930 kgkg , are launched...

Two Earth satellites, A and B, each of mass mmm = 930 kgkg , are launched into circular orbits around the Earth's center. Satellite A orbits at an altitude of 4000 kmkm , and satellite B orbits at an altitude of 12600 kmkm What are the potential energies of the two satellites? (in Jules) What are the kinetic energies of the two satellites? (in Jules) How much work would it require to change the orbit of satellite A to match...

Two satellites are in circular orbits around the earth. The orbit for satellite A is at...

Two satellites are in circular orbits around the earth. The orbit for satellite A is at a height of 555 km above the earth’s surface, while that for satellite B is at a height of 778 km. Find the orbital speed for (a) satellite A and (b) satellite B.

Two satellites are in circular orbits around the earth. The orbit for satellite A is at...

Two satellites are in circular orbits around the earth. The orbit for satellite A is at a height of 458 km above the earth’s surface, while that for satellite B is at a height of 732 km. Find the orbital speed for (a) satellite A and (b) satellite B.

Two satellites, A and B, both of mass m = 115 kg, move in the same...

Two satellites, A and B, both of mass m = 115 kg, move in the same circular orbit of radius r = 7.57 106 m around Earth but in opposite senses of rotation and therefore on a collision course. a) What is the total mechanical energy EA + EB of the two satellites + Earth system before the collision? b)If the collision is completely inelastic so that the wreckage remains as one piece of tangled material (mass = 2m), what...

Synchronous communication satellites are placed in a circular orbit that is 1.88 × 108 m above...

Synchronous communication satellites are placed in a circular orbit that is 1.88 × 108 m above the surface of the earth. What is the magnitude of the acceleration due to gravity at this distance?

A satellite of mass 1,500 kg is placed in a circular Earth orbit at a height,...

A satellite of mass 1,500 kg is placed in a circular Earth orbit at a height, h, above the surface. It is launched from Treasure Island in the SF Bay at 37 degrees latitude (north of the equator). 2465.98 10 , 6.37 10EarthEarthMxkgRx==ma) Derive Kepler’s Thrid Law from Newton’s Universal Law of gravity. b) If the orbital period of the satellite is 12 hrs, find the distance h above the Earth. c) What is the minimum energy required to put...

An object of mass m is in a circular orbit another heavier object of mass M....

An object of mass m is in a circular orbit another heavier object of mass M. The radius of the orbit is R. (a) Derive the speed of the orbiting object. (b) Use this speed to derive the period of the circular orbit. (c) Use your answer and the provided value to determine the period of Earth’s orbit around the Sun based on our simplified circular motion model. Compare this to the actual value which you can look up. Use...

Earth Satellites Table of Earth Satellites ISS Hubble GPS Geosynchronous satellite Moon h (miles); height above...

Earth Satellites Table of Earth Satellites ISS Hubble GPS Geosynchronous satellite Moon h (miles); height above earth's surface 248 12550 r (m) 54.5 3.85 x 108 v(m/s) 7.56 x 103 T(s); period 4.32 x 104 8.62 x 104 days/revolution 1.0 Revolutions/day 1.0

An asteroid, whose mass is 4.90×10-4 times the mass of Earth, revolves in a circular orbit...

An asteroid, whose mass is 4.90×10-4 times the mass of Earth, revolves in a circular orbit around the Sun at a distance that is 6 times the Earth's distance from the Sun. Calculate the period of revolution of the asteroid. Tries 0/10 What is the ratio of the kinetic energy of the asteroid to the kinetic energy of Earth?

Subjects