Now, assume that this rocket can burn a fraction A = 0.8 of its initial fuel mass mo (that is, assume 80% of the total mass is fuel). For k/b = {0.1, 0.5, 1}, compute USING MATHEMATICA the maximum distance Xmax traveled by the rocket before it depletes its fuel reservoir, assuming vex = 2550 ft sec-1 and a burn time of 0.6 s (typical for an Estes Model Rocket).

College Physics
11th Edition
ISBN:9781305952300
Author:Raymond A. Serway, Chris Vuille
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Chapter1: Units, Trigonometry. And Vectors
Section: Chapter Questions
Problem 1CQ: Estimate the order of magnitude of the length, in meters, of each of the following; (a) a mouse, (b)...
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use mathematica to find the maximum distance xmax with those given valus.  SPEED M DONE WITH IT 

mů = -mv + Fext_
(3.29)
3.14 ** Consider a rocket subject to a linear resistive force, f = –bv, but no other external forces. Use
Equation (3.29) in Problem 3.11 to show that if the rocket starts from rest and ejects mass at a constant
rate k = -m, then its speed is given by
I'M DONE WITH THIS
k
b/k
m
SOLVE BELO W ONE
V =
Vex |1-
b
Now, assume that this rocket can burn a fraction A = 0.8 of its initial fuel mass mo (that is, assume 80%
of the total mass is fuel). For k/b = {0.1, 0.5, 1}, compute USING MATHEMATICA the maximum distance
Xmax traveled by the rocket before it depletes its fuel reservoir, assuming vex = 2550 ft sec-1 and a
burn time of 0.6 s (typical for an Estes Model Rocket).
Transcribed Image Text:mů = -mv + Fext_ (3.29) 3.14 ** Consider a rocket subject to a linear resistive force, f = –bv, but no other external forces. Use Equation (3.29) in Problem 3.11 to show that if the rocket starts from rest and ejects mass at a constant rate k = -m, then its speed is given by I'M DONE WITH THIS k b/k m SOLVE BELO W ONE V = Vex |1- b Now, assume that this rocket can burn a fraction A = 0.8 of its initial fuel mass mo (that is, assume 80% of the total mass is fuel). For k/b = {0.1, 0.5, 1}, compute USING MATHEMATICA the maximum distance Xmax traveled by the rocket before it depletes its fuel reservoir, assuming vex = 2550 ft sec-1 and a burn time of 0.6 s (typical for an Estes Model Rocket).
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