An 825 kg space vehicle is circling Earth in a circular orbit with a radius of 10,300 km. Its...
Question 3 1 pts A spacecraft with mass 1,976 kg is in circular orbit around Earth as shown with the green circle in the figure, at an altitude h = 608 km. At point Pin the orbit (see figure), the spacecraft reduces its speed by 4%, causing it to be in an elliptical orbit. What is the semi-major axis of the elliptical orbit in km? Reminder the radius of the orbit is the altitude plus Re, the radius of Earth....
The space shuttle is in a 150 km -high circular orbit. It needs to reach a 680 km -high circular orbit to catch the Hubble Space Telescope for repairs. The shuttle's mass is 7.00×10^4 kg . How much energy is required to boost it to the new orbit? I keep getting the answer of 7.25e13 J, but this is incorrect.
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 507 kg satellite is in a circular orbit at an altitude of 754 km above a planet’s surface. This planet is similar to our Earth. Because of air friction, the satellite eventually is brought to the Earth’s surface, and it hits the Earth with a speed of 3 km/s. The radius of the planet is 7 × 106 m and its mass is 8 × 1024 kg. The gravitational constant is 6.67259 × 10−11 N m2 /kg2. How much...
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...
1. An international space station in the circular orbit at 5500 km above the Earth surface needs to change its orbit to escape from cosmic debris. Find the new orbital altitude for two possible orbits: a) where its speed is increased v=1.1vo or b) its period: is decreased T-0.9T.
The International Space Station typically travels in a circular orbit at an altitude of 400 km above the Earth's surface. The Earth itself has a radius of about 6400 km. Assume that the space station travels in a circular orbit at constant speed (this is a perfectly reasonable assumption). A. Given that the value of g is 8.68m/s28.68m/s2at an altitude of 400 km, determine the value of the space station's speed in its circular orbit. _______ m/s B. At this...
A spacecraft of mass m = 1900 kg is moving on a circular orbit about the earth at a constant speed v = 5.12 km/s. [Given: Mass of the earth M = 5.98 times 10^24 kg, radius of the earth R = 6.37 times10^6 m, gravitational constant G = 6.67 times 10^-11 N.m^2/kg^2.] a. Determine the radius r of the circular orbit. b. What is the period T of the orbit? c. The satellite, by firing its engines, moves to...
A spacecraft with mass 1500 kg is in a circular orbit at an altitude 200 km above the surface of Earth. A) Use the Law of Universal Gravitation and Newton's 2nd law for circular motion to derive and find the speed of the spacecraft in this orbit. B) How much mechanical energy does the spacecraft have in this orbit? C) How much work must the spacecraft engines perform to get it into the above circular orbit from the surface of...
The space shuttle releases a satellite into a circular orbit 640 km above the Earth. Part A How fast must the shuttle be moving (relative to Earth) when the release occurs? v = m/s