Question

Scientists want to place a 2600 kg satellite in orbit around Mars. They plan to have...

Scientists want to place a 2600 kg satellite in orbit around Mars. They plan to have the satellite orbit at a speed of 2439 m/s in a perfectly circular orbit. Here is some information that may help solve this problem:

mmars = 6.4191 x 1023 kg
rmars = 3.397 x 106 m
G = 6.67428 x 10-11 N-m2/kg2

1) What radius should the satellite move at in its orbit? (Measured frrom the center of Mars.)

Homework Answers

Answer #1

#Hi, if you are happy and find this useful please thumbs up. In case, if you have any query regarding the solution please let me know in the comments section below. We can discuss. Thanks!!

Know the answer?
Your Answer:

Post as a guest

Your Name:

What's your source?

Earn Coins

Coins can be redeemed for fabulous gifts.

Not the answer you're looking for?
Ask your own homework help question
Similar Questions
Scientists want to place a 2700 kg satellite in orbit around Mars. They plan to have...
Scientists want to place a 2700 kg satellite in orbit around Mars. They plan to have the satellite orbit a distance equal to 2.4 times the radius of Mars above the surface of the planet. Here is some information that will help solve this problem: mmars = 6.4191 x 1023 kg rmars = 3.397 x 106 m G = 6.67428 x 10-11 N-m2/kg2 1)What is the force of attraction between Mars and the satellite? 2)What speed should the satellite have...
Scientists want to place a 3400 kg satellite in orbit around Mars. They plan to have...
Scientists want to place a 3400 kg satellite in orbit around Mars. They plan to have the satellite orbit a distance equal to 1.5 times the radius of Mars above the surface of the planet. Here is some information that will help solve this problem: mmars = 6.4191 x 1023 kg rmars = 3.397 x 106 m G = 6.67428 x 10-11 N-m2/kg2 1)What is the force of attraction between Mars and the satellite? 2)What speed should the satellite have...
Scientists want to place a 3200 kg satellite in orbit around Mars. They plan to have...
Scientists want to place a 3200 kg satellite in orbit around Mars. They plan to have the satellite orbit a distance equal to 2.1 times the radius of Mars above the surface of the planet. Here is some information that will help solve this problem: mmars = 6.4191 x 1023 kg rmars = 3.397 x 106 m G = 6.67428 x 10-11 N-m2/kg2 1. What is the force of attraction between Mars and the satellite? 2. What speed should the...
Scientists want to place a 1000 kg satellite in a circular orbit around Venus. They want...
Scientists want to place a 1000 kg satellite in a circular orbit around Venus. They want the height of the orbit to be three times the radius of Venus. Mvenus = 4.867 x 1024 kg Rvenus = 6.050 x 106 m G = 6.67428 x 10-11 N-m2/kg2 A) What would be the force of gravity between Venus and the satellite? B) What would be the acceleration due to gravity at the satellite’s orbit? C) What would be the orbital speed...
A satellite of mass 1525 kg is in circular orbit around Earth. The radius of the...
A satellite of mass 1525 kg is in circular orbit around Earth. The radius of the orbit of the satellite is equal to 1.5 times the radius of Earth (RE = 6.378*106 m, ME = 5.98*1024 kg, G = 6.67*10-11 Nm2/kg2). (a) Find the orbital period of the satellite? (b) Find the orbital (tangential) velocity of the satellite.  (c) Find the total energy of the satellite?
A satellite is in a circular orbit around the Earth at an altitude of 3.32 106...
A satellite is in a circular orbit around the Earth at an altitude of 3.32 106 m. (a) Find the period of the orbit. (Hint: Modify Kepler's third law so it is suitable for objects orbiting the Earth rather than the Sun. The radius of the Earth is 6.38 106 m, and the mass of the Earth is 5.98 1024 kg.) h (b) Find the speed of the satellite. km/s (c) Find the acceleration of the satellite. m/s2 toward the...
A satellite is in a circular orbit around the Earth at an altitude of 3.84  106 m....
A satellite is in a circular orbit around the Earth at an altitude of 3.84  106 m. (a) Find the period of the orbit. (Hint: Modify Kepler's third law so it is suitable for objects orbiting the Earth rather than the Sun. The radius of the Earth is 6.38  106 m, and the mass of the Earth is 5.98  1024 kg.) h (b) Find the speed of the satellite. km/s (c) Find the acceleration of the satellite. m/s2 toward the center of the...
A satellite is in a circular orbit around the Earth at an altitude of 3.78 106...
A satellite is in a circular orbit around the Earth at an altitude of 3.78 106 m.(Hint: Solve the parts in reverse order.) (a) Find the period of the orbit. h (b) Find the speed of the satellite. (c) Find the acceleration of the satellite. m/s2 toward the center of the earth
A satellite is in a circular orbit around the Earth at an altitude of 1.66 106...
A satellite is in a circular orbit around the Earth at an altitude of 1.66 106 m. (a) Find the period of the orbit (in hrs). (Hint: Modify Kepler's third law: T2 = (4π2/GMS)r3 so it is suitable for objects orbiting the Earth rather than the Sun. The radius of the Earth is 6.38 106 m, and the mass of the Earth is 5.98 1024 kg.) (b) Find the speed of the satellite (in km/s). (c) Find the acceleration of...
A satellite of mass m = 2.00 ×103 kg is launched into a circular orbit of...
A satellite of mass m = 2.00 ×103 kg is launched into a circular orbit of orbital period T = 4.00 hours. Newton's gravitational constant is G = 6.67 ×10−11 N∙m2/kg2, and the mass and radius of the Earth are respectively M⨁ = 5.97 ×1024 kg and r⨁ = 6.37 ×106 m. Answer the following questions. What is the total mechanical energy (kinetic energy + potential energy) of the satellite in orbit? Take the gravitational potential energy of the satellite...
ADVERTISEMENT
Need Online Homework Help?

Get Answers For Free
Most questions answered within 1 hours.

Ask a Question
ADVERTISEMENT