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tnx! 5 A landing craft with mass 1.22*104 kg is in a circular orbit a distance...
A landing craft with mass 12,500 kg is in a circular orbit 6.75×105 m above the surface of a planet. The period of the orbit is 5200 s. The astronauts in the lander measure the diameter of the planet to be 9.60×10^6m. The lander sets down at the north pole of the planet. What is the weight w of an 85.6 kg astronaut as he steps out onto the planet's surface?
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 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 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,...
A satellite has a mass of 6366 kg and is in a circular orbit 4.28 × 105 m above the surface of a planet. The period of the orbit is 1.9 hours. The radius of the planet is 4.27 × 106 m. What would be the true weight of the satellite if it were at rest on the planet’s surface?
A satellite has a mass of 6392 kg and is in a circular orbit 4.88 × 105 m above the surface of a planet. The period of the orbit is 1.7 hours. The radius of the planet is 4.89 × 106 m. What would be the true weight of the satellite if it were at rest on the planet’s surface?
A satellite has a mass of 3410 kg and is in a circular orbit 5.51 x 106 m above the surface of a planet. The period of the orbit is 7.06 hours. The radius of the planet is 4.04 x 106 m. What is the true weight of the satellite when it is at rest on the planet's surface?
A satellite has a mass of 6425 kg and is in a circular orbit 3.80 105 m above the surface of a planet. The period of the orbit is 2.10 hours. The radius of the planet is 4.09 106 m. What would be the true weight of the satellite if it were at rest on the planet's surface?
A satellite of mass 42.5 kg in geosynchronous orbit at an altitude of 3.58 ✕ 104 km above the Earth's surface remains above the same spot on the Earth. Assume its orbit is circular. Find the magnitude of the gravitational force exerted by the Earth on the satellite. Hint: The answer is not 417 N