A rocket has a total mass of 1.01  105 kg and a burnout mass of 1.14  104 kg, including engines, shell and payload. The rocket blasts off from Earth and exhausts all its fuel in 4.31 min, burning the fuel at a steady rate with an exhaust velocity of ve= 4.66  103 m/s. (a) If air friction and gravity are neglected, what is the speed of the rocket at burnout? m/s(b) What thrust does the engine develop at liftoff? N(c) What is the initial acceleration of the rocket if gravity is not neglected? m/s2(d) Estimate the speed at burnout if gravity isn't neglected. m/s

Principles of Physics: A Calculus-Based Text
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Chapter8: Momentum And Collisions
Section: Chapter Questions
Problem 46P: A rocket has total mass Mi = 360 kg, including Mfuel = 330 kg of fuel and oxidizer. In interstellar...
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A rocket has a total mass of 1.01  105 kg and a burnout mass of 1.14  104 kg, including engines, shell and payload. The rocket blasts off from Earth and exhausts all its fuel in 4.31 min, burning the fuel at a steady rate with an exhaust velocity of ve= 4.66  103 m/s.

(a) If air friction and gravity are neglected, what is the speed of the rocket at burnout?
 m/s

(b) What thrust does the engine develop at liftoff?
 N

(c) What is the initial acceleration of the rocket if gravity is not neglected?
 m/s2

(d) Estimate the speed at burnout if gravity isn't neglected.
 m/s
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