Question

In: Physics

If a satellite is in a sufficiently low orbit, it will encounter air drag from the...

If a satellite is in a sufficiently low orbit, it will encounter air drag from the earth's atmosphere. Since air drag does negative work (the force of air drag is directed opposite the motion), the mechanical energy will decrease. If E decreases (becomes more negative), the radius r of the orbit will decrease. If air drag is relatively small, the satellite can be considered to be in a circular orbit of continually decreasing radius.

a.) A satellite with mass 2140 kg is initially in a circular orbit a distance 330 km above the earth's surface. Due to air drag, the satellite's altitude decreases to 205 km . Calculate the initial orbital speed.

b.) Calculate the increase in orbital speed.

c.) Calculate the initial mechanical energy.

d.) Calculate the change in kinetic energy.

e.) Calculate the change in gravitational potential energy.

f.) Calculate the change in mechanical energy.

g.) Calculate the work done by the force of air drag.

Solutions

Expert Solution

genius_generous answered 6 months ago
Next > < Previous

Related Solutions

If a satellite is in a sufficiently low orbit, it will encounter air drag from the...
If a satellite is in a sufficiently low orbit, it will encounter air drag from the earth's atmosphere. Since air drag does negative work (the force of air drag is directed opposite the motion), the mechanical energy will decrease. If Edecreases (becomes more negative), the radius r of the orbit will decrease. If air drag is relatively small, the satellite can be considered to be in a circular orbit of continually decreasing radius. Part A A satellite with mass 2590...
If a satellite is in a sufficiently low orbit, it will encounter air drag from the...
If a satellite is in a sufficiently low orbit, it will encounter air drag from the earth's atmosphere. Since air drag does negative work (the force of air drag is directed opposite the motion), the mechanical energy will decrease. If E decreases (becomes more negative), the radius r of the orbit will decrease. If air drag is relatively small, the satellite can be considered to be in a circular orbit of continually decreasing radius. a.) A satellite with mass 2250...
A satellite is in an elliptical orbit around the earth. The distance from the satellite to...
A satellite is in an elliptical orbit around the earth. The distance from the satellite to the center of the earth ranges from 7.2 Mm at perigee (where the speed is 8.0 km/s) to 9.9 Mm at apogee. 1. Assume the initial conditions are x = 0, y = 7.2 × 106 m, vx = 8.0×103 m/s, and vy = 0. Use python program to print its speed, distance from the earth, kinetic energy, potential energy, and total mechanical energy...
A satellite is put into an elliptical orbit around the Earth. When the satellite is at...
A satellite is put into an elliptical orbit around the Earth. When the satellite is at its perigee, its nearest point to the Earth, its height above the ground is hp=215.0 km,hp=215.0 km, and it is moving with a speed of vp=8.450 km/s.vp=8.450 km/s. The gravitational constant GG equals 6.67×10−11 m3⋅kg−1⋅s−26.67×10−11 m3·kg−1·s−2 and the mass of Earth equals 5.972×1024 kg.5.972×1024 kg. When the satellite reaches its apogee, at its farthest point from the Earth, what is its height haha above...
A satellite is put into an elliptical orbit around the Earth. When the satellite is at...
A satellite is put into an elliptical orbit around the Earth. When the satellite is at its perigee, its nearest point to the Earth, its height above the ground is ℎp=215.0 km, and it is moving with a speed of ?p=8.850 km/s. The gravitational constant ? equals 6.67×10−11 m3·kg−1·s−2 and the mass of Earth equals 5.972×1024 kg. When the satellite reaches its apogee, at its farthest point from the Earth, what is its height ℎa above the ground? For this...
A satellite is put into an elliptical orbit around the Earth. When the satellite is at...
A satellite is put into an elliptical orbit around the Earth. When the satellite is at its perigee, its nearest point to the Earth, its height above the ground is hp=215.0 km,hp=215.0 km, and it is moving with a speed of vp=8.450 km/s.vp=8.450 km/s. The gravitational constant GG equals 6.67×10−11 m3⋅kg−1⋅s−26.67×10−11 m3·kg−1·s−2 and the mass of Earth equals 5.972×1024 kg.5.972×1024 kg. When the satellite reaches its apogee, at its farthest point from the Earth, what is its height haha above...
A communications satellite is in a synchronous orbit that is 3.47
A communications satellite is in a synchronous orbit that is 3.47
Explain two reasons behind the commercial failure of Low Earth Orbit satellite mobile communications companies (such...
Explain two reasons behind the commercial failure of Low Earth Orbit satellite mobile communications companies (such as Iridium).
A rocket carrying a new 990-kg satellite into orbit misfires and places the satellite in an...
A rocket carrying a new 990-kg satellite into orbit misfires and places the satellite in an orbit with an altitude of 120 km, well below its operational altitude in low-Earth orbit. (a) What would be the height of the satellite's orbit if its total energy were 545 MJ greater? km (b) What would be the difference in the system's kinetic energy? (Include the sign of the value in your answer.) MJ (c) What would be the difference in the system's...
The physics of satellite motion around Jupiter. A 155 kg satellite is placed in orbit 6.00...
The physics of satellite motion around Jupiter. A 155 kg satellite is placed in orbit 6.00 x 105 m above the surface of Jupiter. The tangential speed of the satellite is 3.99 x 104 m/s. Jupiter has a mass of 1.90 x 1027 kg and a radius of 7.14 x 107 m. Determine the radius of motion of the satellite. Calculate the centripetal force acting on the satellite to maintain its orbit. What is the cause of this centripetal force?...
ADVERTISEMENT
Subjects
ADVERTISEMENT
Latest Questions
ADVERTISEMENT