Angular Momentum difficult problem

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Homework Help Overview

The problem involves a space capsule rotating about its longitudinal axis at a specified rate, with the goal of stopping this rotation using jets that eject gas. The context includes calculations related to angular momentum, moment of inertia, and the effects of torque from the jets.

Discussion Character

  • Mixed

Approaches and Questions Raised

  • Participants discuss the initial conditions and parameters, including angular velocity, moment of inertia, and gas ejection rate. There are attempts to apply given formulas, but some participants express confusion regarding the dimensions and correctness of the equations provided.

Discussion Status

There are multiple interpretations of the problem and the equations involved. Some participants have reported different results using various approaches, leading to discussions about the validity of the formulas and the assumptions made. Guidance has been offered regarding the calculation of torque and angular acceleration, but no consensus has been reached on the correct method.

Contextual Notes

Participants note discrepancies in the results obtained from different equations and the potential impact of the number of jets on the calculations. There is also mention of a prior solution from 2007 that remains unclear to some participants.

Arshad_Physic
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Homework Statement



The rear view of a space capsule that is rotating about its longitudinal axis is 3rev/min. The occupants want to stop this rotation. They have small jets mounted tangentially at a distance 1.2 m from the axis, as indicated, and can eject 8 g/s of gas from each jet with a nozzle velocity of 591 m/s. The moment of inertia of the ship about its axis (assumed to be constant is 2200 kg m2.

Homework Equations



This is the final equation my professor gave: t= [L (initial)]/ ((m/t)*R*V)^2

Also, L(initial) = Iw


The Attempt at a Solution



Hello. My computer generated homework gave 10 questions. I was able to solve 9 of them, but this one seems IMPOSSIBLE! lol :) I know that this has been solved in Physics forums in April 2007, but it doesn't makes sense to me :(

I tried to understand what professor told me as to HOW to solve this problem. But I just didn't get it. Even worse, I tried plugging in the answer and I didn't get it right lol.


I know that

w = 3rev/s * 2pi * 1/60 = pi/10 rad/sec

L(initial) is Iw = 2200*

m/t = 8g/s = 0.008 kg/s

R=1.2m

V = 591 m/s

But when I plug in the equations I just get the WRONG answer :(

I THINK that the problem is with the part that I plug in 0.008 kg/s for the part in the equation where I am supposed to plug in m/t.

Please helP!

Thanks! :)

Arshad
 
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t= [L (initial)]/ ((m/t)*R*V)^2
The dimensions don't seem to work out in this formula!
Using the linear/rotational analogy, if you start with the impulse formula
Ft = p
τt = L
t = L/τ = L/(m/t*R*v)
you get the same formula but without the square.
 
I get answer t = 122 secs using the equation you give, which is wrong. The equation my professor gave is wrong too, for I get answet t = about 21 seconds.

I got some help, and I got the right answer. We first find Torque. Divide the torque by Inertia to get angular acceleration. Using that we plug it into the equation 0=wi+0.5At^2, where A = angular acceleration.

My answer turned out to be t = 60.something and the program thingy accepted it! :)

THanks for your help though, very much! :)
 
Thanks for the report! Always nice to see how it turns out. But I'm puzzled because "0=wi+0.5At^2" is not a valid formula - should be 0 = wi+αt, which should give the same answer as our
t = L/τ = L/(m/t*R*v)
You don't say how many rockets there are, but if there are 2, we get
t = I*ω/(m/t*R*v)
= 2200*3(2π)/60 all divided by (2*.008*1.2*591)
= 60.9 seconds.
 

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