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show work with an atmospheric detection satellite orbiting in a circular orbit at a radius R...
A satellite in a circular orbit with radius 15000 mi (measured from the center of the planet) orbits the planet with a speed of 16000 m/s. A second satellite orbits the same planet in a circular path of radius 7090 mi. What is its approximate orbital speed? 4. 33. d) 23000 m/s B7-FPT# b) 8000 m/s a) 4000 m/s e) Not enough information - we need the masses of the satellites. c) 11000 m/s
A 270 kg satellite is orbiting on a circular orbit 6180 km above the Earth's surface. Determine the speed of the satellite. (The mass of the Earth is 5.97×1024 kg, and the radius of the Earth is 6370 km.)
Two satellites are in circular orbits around the earth. The orbit for satellite A is at a height of 364 km above the earth's surface, while that for satellite B is at a height of 880. km. Find the orbital speed for satellite A and satellite B. (a) VA = (b) VB =
A space station is orbiting the Earth. It moves in a circular orbit with a radius equal to three times the Earth's radius. A supply satellite is designed to travel to the station and dock smoothly when it arrives. If the supply satellite is fired as a simple projectile from the Earth's surface, what is the minimum intial speed required for it to reach the space station and have a speed equal to the station's speed when it arrives? Ignore...
Chapter 05, Problem 31 GO Two satellites are in circular orbits around the earth. The orbit for satellite A is at a height of 448 km above the earth's surface, while that for satellite B is at a height of 926 km. Find the orbital speed for (a) satellite A and (b) satellite (a) VA- (b) V- Show Work is REQUIRED for this questions Open Show Work
A 180 kg satellite is orbiting on a circular orbit 6355 km above the Earth's surface. Determine the speed of the satellite. (The mass of the Earth is 5.97x1024 kg, and the radius of the Earth is 6370 km.) Submit Answer Tries 0/12
4. Two satellites (equal in mass) are in a circular orbit around the Earth. Satellite 1 is traveling at constant velocity vi. Satellite B is traveling at constant veloci v2. If Satellite A is at a distance ri from the Earth's center, the distance from Satellite B to the Earth's center is A), Vi
Two identical satellites orbit the earth in stable orbits. One satellite orbits with a speed v at a distance r from the center of the earth. The second satellite travels at a speed that is less than v.At what distance from the center of the earth does the second satellite orbit?At a distance that is less than r.At a distance equal to r.At a distance greater than r.Now assume that a satellite of mass m is orbiting the earth at a distance...
the speed of a satellite (A) is 8,000 m/s orbiting at a distance r from the center of the planet, what would be the speed of another identical satellite (B) if it orbits three times as far from the center of the planet as satellite (A)?
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....