mo The Tsiolkovsky rocket equation is Av = ve In| mf It calculates the maximum possible change in velocity for a rocket based on several parameters. ve is the velocity of the rocket's exhaust gasses (the fire part). mo is the initial mass of the rocket, including its fuel. is the final mass of the rocket once all its fuel has been mf used. Calculate the maximum possible velocity change for a rocket if its exhaust gasses travel 3300 m its initial mass S is 23000kg, and its final mass is 1100kg. Round your answer to the nearest integer. m Δυ

Calculus: Early Transcendentals
8th Edition
ISBN:9781285741550
Author:James Stewart
Publisher:James Stewart
Chapter1: Functions And Models
Section: Chapter Questions
Problem 1RCC: (a) What is a function? What are its domain and range? (b) What is the graph of a function? (c) How...
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(3)
mo
The Tsiolkovsky rocket equation is Av = ve ln
mf
= Ve
It calculates the maximum possible change in velocity for a
rocket based on several parameters.
Ve is the velocity of the rocket's exhaust gasses (the fire
part).
mo is the initial mass of the rocket, including its fuel.
is the final mass of the rocket once all its fuel has been
mf
used.
Calculate the maximum possible velocity change for a
rocket if its exhaust gasses travel 3300-
m
its initial mass
S
is 23000kg, and its final mass is 1100kg. Round your
answer to the nearest integer.
m
Δυ-
m
For reference, a rocket needs Av of about 9400-
in
S
order to acheive orbit around the Earth.
Transcribed Image Text:(3) mo The Tsiolkovsky rocket equation is Av = ve ln mf = Ve It calculates the maximum possible change in velocity for a rocket based on several parameters. Ve is the velocity of the rocket's exhaust gasses (the fire part). mo is the initial mass of the rocket, including its fuel. is the final mass of the rocket once all its fuel has been mf used. Calculate the maximum possible velocity change for a rocket if its exhaust gasses travel 3300- m its initial mass S is 23000kg, and its final mass is 1100kg. Round your answer to the nearest integer. m Δυ- m For reference, a rocket needs Av of about 9400- in S order to acheive orbit around the Earth.
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