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What does the geodesic effect amount to for the axis of the Earth in its orbit...
A satellite of Earth is moving in a circular orbit with Earth at its center, at...
A satellite of Earth is moving in a circular orbit with Earth at its center, at a constant speed of 2.00 km/s. a.) How high is the satellite above the surface of the Earth? b.) How long does it take for the satellite to complete one revolution? Helpful info (but not all of it is relevant!): universal gravitational constant G is = 6.674 x 10^-11 m^3/kg s^2 (units may also be expressed as N m^2/kg^2) Mass of Sun = 1.989...
If your friend weighs 150lbs on the earth what would they weigh while standing on the...
If your friend weighs 150lbs on the earth what would they weigh while standing on the surface of the sun? (Assuming, unrealistically, that they weren’t vaporized of course!) (G = 6.67 × 10-11 N•m 2 /kg2 , R of the sun is 6.955 × 108 m, mass of the sun is 1.989× 1030 kg, 1 ton = 2000 lbs) A. 4 tons. B. 2 tons. C. 1.5 tons. D. 1.5 × 109 tons . E. 1.4 × 1010 tons. Please...
10) The international space station (ISS) orbits the Earth from an altitude of 408 km. a)...
10) The international space station (ISS) orbits the Earth from
an altitude of 408 km.
a) Calculate the strength of Earth’s gravity on the ISS at that
altitude. (Hint: How far is the ISS from the center of mass of the
Earth?)
b) Earth’s gravity is what keeps the ISS in its orbit (which we
will assume is circular). At what speed does the ISS orbit the
Earth?
Please show working
New Equations 2 torque = (lever arm) x (force)...
A satellite is put into an elliptical orbit around the Earth. When the satellite is at its perigee, its nearest point t...
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 = 249.0 km, and it is moving with a speed of up = 7.950 km/s. The gravitational constant G equals 6.67 x 10-11 mº.kg-1.5-2 and the mass of Earth equals 5.972 x 1024 kg. When the satellite reaches its apogee, at its farthest point from the Earth, what is...
If you weigh 660 N on the earth, what would be your weight on the surface...
If you weigh 660 N on the earth, what would be your weight on the surface of a neutron star that has the same mass as our sun and a diameter of 16.0 km ? Take the mass of the sun to be ms = 1.99×1030 kg , the gravitational constant to be G = 6.67×10−11 N⋅m2/kg2 , and the acceleration due to gravity at the earth's surface to be g = 9.810 m/s2 . Express your weight wstar in...
What is the angular kinetic energy of the Earth due to its orbit around the sun?...
What is the angular kinetic energy of the Earth due to its orbit around the sun? In Homework 10, you found the two main angular velocities of the Earth: one due to the Earth's motion around the sun, and one due to its rotation about its own axis. Now let's figure out the energy and momentum associated with that motion. IVO ALV O a ? For the purposes of this problem, treat the Earth as a solid, uniform sphere with...
A satellite is in a circular orbit about the Earth at a distance of four (4)...
A satellite is in a circular orbit about the Earth at a distance of four (4) Earth radii above the surface of the Earth. What is the velocity of the satellite? (Earth's mass: ME = 5.98 x 1024 kg; the radius of the Earth: 6.4 x 106m ; G = 6.67 x 10-11 Nm2/kg2 ). A) 4,072.5 m/s B)3,530.5 m/s C)5,582.2 m/s D)7,465.9 m/s
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 ho = 207.0 km, and it is moving with a speed of v, = 8.050 kr/s. The gravitational constant G equals 6.67 x 10-11 m² kg-15-2 and the mass of Earth equals 5.972 x 1024 kg. When the satellite reaches its apogee, at its farthest point from the Earth, what...
A satellite is in a circular orbit about the earth (ME = 5.98 × 10 24...
A satellite is in a circular orbit about the earth (ME = 5.98 × 10 24 5.98 × 10 24 kg). The period of the satellite is 1.00 × 10 4 1.00 × 10 4 s. What is the speed at which the satellite travels?(G = 6.67 × 10 − 11 6.67 × 10 − 11 N.m2/kg2)
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=227.0 km, and it is moving with a speed of vp=8.950 km/s. The gravitational constant G 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...
10) The international space station (ISS) orbits the Earth from
an altitude of 408 km.
a) Calculate the strength of Earth’s gravity on the ISS at that
altitude. (Hint: How far is the ISS from the center of mass of the
Earth?)
b) Earth’s gravity is what keeps the ISS in its orbit (which we
will assume is circular). At what speed does the ISS orbit the
Earth?
Please show working
New Equations 2 torque = (lever arm) x (force)...
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 = 249.0 km, and it is moving with a speed of up = 7.950 km/s. The gravitational constant G equals 6.67 x 10-11 mº.kg-1.5-2 and the mass of Earth equals 5.972 x 1024 kg. When the satellite reaches its apogee, at its farthest point from the Earth, what is...
What is the angular kinetic energy of the Earth due to its orbit around the sun? In Homework 10, you found the two main angular velocities of the Earth: one due to the Earth's motion around the sun, and one due to its rotation about its own axis. Now let's figure out the energy and momentum associated with that motion. IVO ALV O a ? For the purposes of this problem, treat the Earth as a solid, uniform sphere with...
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 ho = 207.0 km, and it is moving with a speed of v, = 8.050 kr/s. The gravitational constant G equals 6.67 x 10-11 m² kg-15-2 and the mass of Earth equals 5.972 x 1024 kg. When the satellite reaches its apogee, at its farthest point from the Earth, what...
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