Sustainable Energy
1st Edition
ISBN: 9781133108689
Author: Richard A. Dunlap
Publisher: Cengage Learning
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A rocket engine burns 8.5kg of fuel and oxidizer per second, and combinations gases exit the rocket at a velocity of 565m/s relative to the rocket, at a pressure approximately equal to the surrounding atmospheric pressure. Find the thrust produced by the rocket engine.
A 400-kg satellite was placed in a circular orbit 1500 km above the surface of the earth. At this elevation the acceleration of gravity is 6.43 m/s ^ 2 . Determine the kinetic energy of the satellite in kJ, knowing that its orbital speed is 25.6*10^ 3 km/h .
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4 decimal place
Unit: KJ(kilojoules)
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calculate the density and specific weight of carbon dioxide at an absolute pressure of 300 kN/m^2 and 60 degree celsius
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