For the known values of the Earth such that RE = 6.37×106m and ME = 5.97×1024kg,...
For the known values of the Earth such that RE = 6.37×106m and ME = 5.97×1024kg, determine (a) the height that the satellite is orbiting above the surface, and (b) tangential velocity of a satellite while in a geosynchronous orbit. Take a sidereal day to be 23 hours and 56 minutes.
I calculated a to be 35730. I cant figure out how to find b. Thanks!
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For the known values of the Earth such that RE =
6.37×106m and ME = 5.97×1024kg,...
Find the height H of a geosynchronous satellite above the surface of the earth. You may...
Find the height H of a geosynchronous satellite above the surface of the earth. You may well want to find the radius of the orbit R first. You may use the following constants: The universal gravitational constant G is 6.67×10−11Nm2/kg2. The mass of the earth is 5.98×1024kg. The mass of the satellite is 2.10×102kg. The radius of the earth is 6.38×106m. Give the height of the orbit above the surface in km to three significant digits.
Consider a 475 kg satellite in a circular orbit at a distance of 3.06 x 104...
Consider a 475 kg satellite in a circular orbit at a distance of 3.06 x 104 km above the Earth's surface. What is the minimum amount of work W 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 109 km and Me = 5.97 x 1024 kg,...
Consider a 455 kg satellite in a circular orbit at a distance of 3.02 x 104...
Consider a 455 kg satellite in a circular orbit at a distance of 3.02 x 104 km above the Earth's surface. What is the minimum amount of work W 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 % 10% km and Me = 5.97 x 1024 kg,...
Consider a 495 kg satellite in a circular orbit at a distance of 3.02 x 104...
Consider a 495 kg satellite in a circular orbit at a distance of 3.02 x 104 km above the Earth's surface. What is the minimum amount of work W 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,...
Consider a 455 kg satellite in a circular orbit at a distance of 3.02 x 104...
Consider a 455 kg satellite in a circular orbit at a distance of 3.02 x 104 km above the Earth's surface. What is the minimum amount of work W the satellite's thrusters must do to raise the satellite to a geosynchronous orbit? Geosynchronous orbits occur at approximately 3.60 x 107 km above the Earth's surface. The radius of the Earth and the mass of the Earth are RE = 6.37 x 109 km and Me = 5.97 x 1024 kg,...
numbers, the other with the equations. Put a box around the answer to each part. 1....
numbers, the other with the equations. Put a box around the answer to each part. 1. An object's circular orbital velocity vc around the earth can be calculated using the equation ", where ve is the circular orbital velocity, μ-3.98601 E5 km3/s, is the earth's gravitational parameter, and r is the distance of the object from the earth's center. Some commercial satellites, like DirecTV, are in an orbit where they take one sidereal day (23h 56m 4.09s) to orbit the...
For the Earth, the mass ME = 5·96x1024 kg, and the radius RE-6.37x106 m. ) The...
For the Earth, the mass ME = 5·96x1024 kg, and the radius RE-6.37x106 m. ) The escape velocity. (b) If a satellite is launched to orbiting the Earth at a h Find eight of 400 e, what is its orbiting velocity. (15 points for each part)
A geostationary satellite is a satellite located in an orbit such that it remains above the...
A geostationary satellite is a satellite located in an orbit such that it remains above the same point on the Earth’s surface. [Assume it takes 23 hours 56 minutes 4.09 seconds for the Earth to spin around once.] a) What is the angular velocity of such a satellite? b) What is the altitude of such a satellite? c) Calculate the period of a satellite orbiting 200km above the Earth.
An object of mass m moves at a constant speed v in a circular path of radius r.
An object of mass m moves at a constant speed v in a circular path of radius r. The force required to produce the centripetal component of acceleration is called the centripetal force and is given by F=mv2/r. Newton's Law of Universal Gravitation is given by F=GMm/d2, where d is the distance between the centers of the two bodies of masses M and m, and G is a gravitational constant. The speed required for circular motion is v= √(GM/r). Use the...
It takes 23 hours 56 minutes and 4 seconds for the earth to make one revolution...
It takes 23 hours 56 minutes and 4 seconds for the earth to make one revolution (mean sidereal day). What is the angular speed of the earth? The Ang. Speed = 7.29*10^-5 rad/s 1b) Assume the earth is spherical. Relative to someone on the rotation axis, what is the linear speed of an object on the surface if the radius vector from the center of the earth to the object makes an angle of 65.0° with the axis of rotation....
Consider a 475 kg satellite in a circular orbit at a distance of 3.06 x 104 km above the Earth's surface. What is the minimum amount of work W 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 109 km and Me = 5.97 x 1024 kg,...
Consider a 455 kg satellite in a circular orbit at a distance of 3.02 x 104 km above the Earth's surface. What is the minimum amount of work W 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 % 10% km and Me = 5.97 x 1024 kg,...
Consider a 495 kg satellite in a circular orbit at a distance of 3.02 x 104 km above the Earth's surface. What is the minimum amount of work W 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,...
Consider a 455 kg satellite in a circular orbit at a distance of 3.02 x 104 km above the Earth's surface. What is the minimum amount of work W the satellite's thrusters must do to raise the satellite to a geosynchronous orbit? Geosynchronous orbits occur at approximately 3.60 x 107 km above the Earth's surface. The radius of the Earth and the mass of the Earth are RE = 6.37 x 109 km and Me = 5.97 x 1024 kg,...
numbers, the other with the equations. Put a box around the answer to each part. 1. An object's circular orbital velocity vc around the earth can be calculated using the equation ", where ve is the circular orbital velocity, μ-3.98601 E5 km3/s, is the earth's gravitational parameter, and r is the distance of the object from the earth's center. Some commercial satellites, like DirecTV, are in an orbit where they take one sidereal day (23h 56m 4.09s) to orbit the...
For the Earth, the mass ME = 5·96x1024 kg, and the radius RE-6.37x106 m. ) The escape velocity. (b) If a satellite is launched to orbiting the Earth at a h Find eight of 400 e, what is its orbiting velocity. (15 points for each part)
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