A rocket is at rest in space relative to the Earth and has a total mass (including propellant) of M = 2.55 x 105 kg. The engines consume fuel at a constant rate of 480 kg/s, and it leaves the rocket %3D nozzle with an exhaust velocity of 5.35 km/s. If the rocket has a "main burn" for 250 s, what is the change in the rocket's velocity in km/s?

Principles of Physics: A Calculus-Based Text
5th Edition
ISBN:9781133104261
Author:Raymond A. Serway, John W. Jewett
Publisher:Raymond A. Serway, John W. Jewett
Chapter8: Momentum And Collisions
Section: Chapter Questions
Problem 47P: A model rocket engine has an average thrust of 5.26 N. It has an initial mass of 25.5 g, which...
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A rocket is at rest in space relative to the Earth and has a total mass (including propellant) of M =
2.55 x 105 kg. The engines consume fuel at a constant rate of 480 kg/s, and it leaves the rocket
nozzle with an exhaust velocity of 5.35 km/s. If the rocket has a "main burn" for 250 s, what is
the change in the rocket's velocity in km/s?
Transcribed Image Text:A rocket is at rest in space relative to the Earth and has a total mass (including propellant) of M = 2.55 x 105 kg. The engines consume fuel at a constant rate of 480 kg/s, and it leaves the rocket nozzle with an exhaust velocity of 5.35 km/s. If the rocket has a "main burn" for 250 s, what is the change in the rocket's velocity in km/s?
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