Question

A rocket with mass 6.00×103 kg is in a circular orbit of radius 7.10×106 m around...

A rocket with mass 6.00×103 kg is in a circular orbit of radius 7.10×106 m around the earth. The rocket's engines fire for a period of time to increase that radius to 8.90×106 m , with the orbit again circular.

What is the change in the rocket's kinetic energy? Does the kinetic energy increase or decrease?

Express your answer with the appropriate units. Enter positive value if the kinetic energy increases and negative value if the kinetic energy decreases.

What is the change in the rocket's gravitational potential energy? Does the potential energy increase or decrease?

Express your answer with the appropriate units. Enter positive value if the gravitational potential energy increases and negative value if the gravitational potential energy decreases.

How much work is done by the rocket engines in changing the orbital radius?

Express your answer with the appropriate units.

Homework Answers

Answer #1

The answer is given below. Please upvote

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
A rocket with mass 5.00×103 kg is in a circular orbit of radius 7.50×106 m around...
A rocket with mass 5.00×103 kg is in a circular orbit of radius 7.50×106 m around the earth. The rocket's engines fire for a period of time to increase that radius to 8.70×106 m , with the orbit again circular. What is the change in the rocket's kinetic energy? Does the kinetic energy increase or decrease? What is the change in the rocket's gravitational potential energy? Does the potential energy increase or decrease? Express your answer with the appropriate units....
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...
Approximate Mars's orbit as circular with a radius equal to semimajor axis of the real orbit....
Approximate Mars's orbit as circular with a radius equal to semimajor axis of the real orbit. Part A What is the magnitude of the gravitational force exerted by the Sun on Mars? Express your answer to two significant digits and include the appropriate units. Part B What is the magnitude of the gravitational force exerted by Mars on the Sun? Express your answer to two significant digits and include the appropriate unit
A satellite of mass m is in an elliptical orbit around the Earth, which has mass...
A satellite of mass m is in an elliptical orbit around the Earth, which has mass Me and radius Re. The orbit varies from closest approach of distance a at point A to maximum distance of b from the center of the Earth at point B. At point A, the speed of the satellite is v0. Assume that the gravitational potential energy Ug = 0 when masses are an infinite distance apart. Express your answers in terms of some or...
A spacecraft of 150 kg mass is in a circular orbit about the Earth at a...
A spacecraft of 150 kg mass is in a circular orbit about the Earth at a height h = 5RE. (a) What is the period of the spacecraft's orbit about the Earth? T = answer in hours (b) What is the spacecraft's kinetic energy? K = Units in J (c) Express the angular momentum L of the spacecraft about the center of the Earth in terms of its kinetic energy K. (Use the following as necessary: RE for the radius...
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 in a circular orbit around the earth with a radius 1.019 times the mean...
A satellite in a circular orbit around the earth with a radius 1.019 times the mean radius of the earth is hit by an incoming meteorite. A large fragment (m = 95.0 kg) is ejected in the backwards direction so that it is stationary with respect to the earth and falls directly to the ground. Its speed just before it hits the ground is 375.0 m/s. (1)  Find the total work done by gravity on the satellite fragment. RE 6.37·103 km;...
1.Zero, a hypothetical planet, has a mass of 4.9 x 1023 kg, a radius of 3.3...
1.Zero, a hypothetical planet, has a mass of 4.9 x 1023 kg, a radius of 3.3 x 106 m, and no atmosphere. A 10 kg space probe is to be launched vertically from its surface. (a) If the probe is launched with an initial kinetic energy of 5.0 x 107 J, what will be its kinetic energy when it is 4.0 x 106 m from the center of Zero? (b) If the probe is to achieve a maximum distance of...
Consider a satellite of mass m in a circular orbit of radius r around the Earth...
Consider a satellite of mass m in a circular orbit of radius r around the Earth of mass ME and radius RE. 1. What is the gravitational force (magnitude and direction) on the satellite from Earth? 2. If we define g(r) to be the force of gravity on a mass m at a radial distance r from the center of the Earth, divided by the mass m, then evaluate the ratio g(r)/g(RE)to see how g varies with radial distance. If...
In a shuttle craft of mass m = 1900 kg, Captain Janeway orbits a planet of...
In a shuttle craft of mass m = 1900 kg, Captain Janeway orbits a planet of mass M = 5.98×1024 kg, in a circular orbit of radius r = 6.80×106 m. Janeway briefly fires a forwardpointing thruster, reducing her speed by 4.6percent.(Assume that there was a negligible change in the mass of the craft). Just then, what are ... (e) the gravitational potential energy (f) the mechanical energy of the shuttle craft (g) What is the semimajor axis of the...