A satellite is executing a circular orbit around the Earth (M = 5.98x1024 kg) with an orbital speed of 7700 m/s. What is the value of g at this orbital radius?
orbital speed = sqrt(GM/R)
where G = gravitational constant
M = mass of the earth
R = radius
7700 = sqrt(6.67*10^-11*5.98*10^24 / R)
R = 6.727*10^6 m
g = GM/R^2
= 6.67*10^-11*5.98*10^24 / (6.727*10^6)^2
= 8.81 m/s^2
so second option 8.8 m/s^2 is the correct answer
A satellite is executing a circular orbit around the Earth (M = 5.98x1024 kg) with an...
Find the speed of a satellite in a circular orbit around the Earth with a radius 2.77 times the mean radius of the Earth. (Radius of Earth -6.37x103 km, mass of Earth 5.98x1024 kg, G - 6.67x10 11 Nm2/kg2.)
A satellite is in a circular orbit around the Earth at an altitude of 2.52 106 m. (a) Find the period of the orbit. (Hint: Modify Kepler's third law: T2 =(4π^2/GMs)r^3 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....
A particular satellite was placed in a circular orbit about 163 mi above Earth. (a) Determine the orbital speed of the satellite. m/s (b) Determine the time required for one complete revolution. min 1024 kg.) An artificial satellite circling the Earth completes each orbit in 119 minutes. (The radius of the Earth is 6.38 x 106 m. The mass of the Earth is 5.98 (a) Find the altitude of the satellite. m (b) What is the value of g at...
A satellite is in a circular orbit around the Earth at an altitude of 2.24 x 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 x 106 m, and the mass of the Earth is 5.98 x 1024 kg.) h (b) Find the speed of the satellite. km/s (c) Find the acceleration of the satellite....
A 544-kg satellite is in a circular orbit about Earth at a height above Earth equal to Earth's mean radius. (a) Find the satellite's orbital speed. m/s (b) Find the period of its revolution. (c) Find the gravitational force acting on it A satellite of Mars, called Phobos, has an orbital radius of 9.4 x 106 m and a period of 2.8 104 s. Assuming the orbit is circular, determine the mass of Mars. x 10 s. Assuming kg
A satellite in circular orbit around the earth has an orbital speed of 6.2 km/s. What is the period of the orbit? Assume the mass of the Earth is 5.98e24 kg.
4. A 1000-kg satellite in circular orbit around the Earth is moving at a speed of 7 x 10 m/s. How much work must be done to "raise" the satellite to a higher circular orbit doubling its height above the surface of the Earth?
please refer to picture
A satellite is in a circular orbit around the Earth. To increase the speed of the satellite while maintaining a circular orbit, one would need to a. b. c. d. increase in the satellite's mass. decrease in the satellite's mass. increase in the satellite's orbital radius. decrease the satellite's orbital radius. none of the above.
A satellite is in a circular orbit around an unknown planet. The satellite has a speed of 1.95 x 104 m/s, and the radius of the orbit is 3.72 x 106 m. A second satellite also has a circular orbit around this same planet. The orbit of this second satellite has a radius of 7.51 x 106 m. What is the orbital speed of the second satellite?
A satellite is in a circular orbit around an unknown planet. The satellite has a speed of 1.15 x 104 m/s, and the radius of the orbit is 2.71 x 106 m. A second satellite also has a circular orbit around this same planet. The orbit of this second satellite has a radius of 9.05 x 106 m. What is the orbital speed of the second satellite?