Question

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 = 69.0 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 367.0 m/s.

a)Find the total work done by gravity on the satellite fragment. RE 6.37·103 km; Mass of the earth= ME 5.98·1024 kg.

b)Calculate the amount of that work converted to heat.

Homework Answers

Answer #1

a) radius of satellite r = 1.019 x 6.37e6 m = 6.49e6 m

Escape velocity from the surface of earth is V = √(GM/R) = √(3.98e14/6.49e6) = 7831 m/s

The momentum of the fragment is 69x7831 = 540000 kgm/s

Now we need the change in PE between the orbital height and ground.

Gravitational potential energy (to center of earth)
PE = G m₁m₂/r
ΔPE = (GMm)(1/r₁ – 1/r₂)
ΔPE = (3.98e14•69)(1/6.49e6 – 1/6.37e6)
ΔPE = (2.74e16)(1.54e-7 – 1.570e-7)
ΔPE = 8.22e7 J (total work)

b) KE = ½mV²
½(69)V² = 8.22e7
V = 1543 m/s

but actual velocity is 367 m/s or a KE of
KE = ½(69)(367)² = 4.65e6 J

difference is in heat
ΔKE = 8.22e7 J – 4.65e6 J = 3.57e7 J

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 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;...
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 4,000 kg satellite is traveling in a circular orbit 200 km above the surface of...
A 4,000 kg satellite is traveling in a circular orbit 200 km above the surface of the Earth. A 30.0 gram marble is dropped inside the satellite. What is the force of gravity on the marble as viewed by the observers on the Earth? (ME = 5.98 × 1024 kg, RE = 6.37 × 106 m, G = 6.67 × 10−11 N·m2/kg2) A 5,000 kg satellite is orbiting the Earth in a circular path. The height of the satellite above...
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 1.52 106...
A satellite is in a circular orbit around the Earth at an altitude of 1.52 106 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 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 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 200 kg satellite is placed in Earth’s orbit 200 km above the surface. The Radius...
A 200 kg satellite is placed in Earth’s orbit 200 km above the surface. The Radius of Earth is 6.37 x 106 m, and the Earth’s mass is 5.98 x 1024 kg. A) Assuming a circular orbit, how long does the satellite take to complete one orbit? B) What is the satellite’s speed?
Consider a 355kg satellite in a circular orbit at a distance of 3.07 x 104 km...
Consider a 355kg satellite in a circular orbit at a distance of 3.07 x 104 km above the Earth’s surface. What is the minimum amount of work the satellite’s thrusters must do to raise the satellite to a geosynchronous orbit? Geosynchronous orbits occur at approximately 3.60 x 104 km above the Earth’s surface. The radius of the Earth and the mass of the Earth are RE = 6.37 x 103 km and ME = 5.97 x 1024 kg respectively. The...
How fast is a satellite moving if it is in a circular orbit whose radius is...
How fast is a satellite moving if it is in a circular orbit whose radius is 22000 km? G = 6.67 x 10-11 Nm2/kg2, and the mass of the earth is 5.98 x 1024 kg.