Question
In: Physics
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?
- In what direction is the centripetal force always acting?
Solutions
genius_generous answered 2 years agoRelated Solutions
The physics of satellite motion around Jupiter. A satellite is placed in orbit 5.00 x 105...
The physics of satellite motion around Jupiter.
A satellite is placed in orbit 5.00 x 105 m above the
surface of Jupiter. Jupiter has a mass of 1.80 x 1027 kg
and a radius of 8.14 x 107 m.
Determine the radius of motion of the satellite.
What force is providing the centripetal force necessary for the
satellite to stay in orbit?
In what direction is the centripetal force always acting?
Derive the mathematical equation that allows you to calculate...
A satellite of mass 2.00 x 104 kg is placed in orbit around Jupiter. The mass...
A satellite of mass 2.00 x 104 kg is placed in orbit
around Jupiter. The mass of Jupiter is 1.90 x 1027 kg.
The distance between the satellite and the centre of Jupiter is
7.24 x 107 m.
Determine the force of gravitational attraction
(Fg) between the satellite and Jupiter.
One of the moons of Jupiter is Io. The distance between the
centre of Jupiter and the centre of Io is 4.22 x 108 m.
If the force of gravitational...
A satellite is placed in an elongated elliptical (not circular) orbit around the Earth. At the...
A satellite is placed in an elongated elliptical (not circular)
orbit around the Earth. At the point in its orbit where it is
closest to the Earth, it is a distance of 1.00 × 10^6
m from the surface (not the center) of the Earth,
and is moving at a velocity of 5.14 km/s. At the
point in its orbit when it is furthest from the Earth it is a
distance of 2.00×10^6 m from the surface of the
Earth....
A satellite of mass 220 kg is placed into Earth orbit at a height of 150...
A satellite of mass 220 kg is placed into Earth orbit at a
height of 150 km above the surface.
(a) Assuming a circular orbit, how long does the satellite take
to complete one orbit?
h
(b) What is the satellite's speed?
m/s
(c) Starting from the satellite on the Earth's surface, what is the
minimum energy input necessary to place this satellite in orbit?
Ignore air resistance but include the effect of the planet's daily
rotation.
J
A satellite of mass 180 kg is placed into Earth orbit at a height of 850...
A satellite of mass 180 kg is placed into Earth orbit at a
height of 850 km above the surface.
(a) Assuming a circular orbit, how long does the satellite take
to complete one orbit?
ans)_____h
(b) What is the satellite's speed?
7558.5 Correct: Your answer is correct. m/s
(c) Starting from the satellite on the Earth's surface, what is
the minimum energy input necessary to place this satellite in
orbit? Ignore air resistance but include the effect of the...
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...
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 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...
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