Postion of an object at a given time?

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Homework Help Overview

The discussion revolves around a problem involving the position of a rocket that accelerates straight upward from rest with a constant net acceleration until its fuel is exhausted. Participants are analyzing the equations of motion and the implications of the rocket's height at specific times.

Discussion Character

  • Exploratory, Mathematical reasoning, Problem interpretation

Approaches and Questions Raised

  • Participants discuss the application of kinematic equations to determine the rocket's position and height at the moment the fuel is burnt. There is a focus on the numerical factors involved in the calculations and the interpretation of the problem requirements.

Discussion Status

The discussion is ongoing, with participants exploring different interpretations of the problem. Some have provided calculations and questioned the accuracy of their results, while others suggest further steps to find the maximum height after fuel exhaustion.

Contextual Notes

There is mention of specific requirements for expressing the answer numerically in meters and potential confusion regarding the expected format for responses. Participants are also considering the effects of gravity on the rocket's motion after fuel is burnt.

badman
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im trying to do this problem involving the postion of a rocket going straight up at a given time.

it says a rocket initially at rest on the ground, accelerates straight upward from rest with constant net acceleration a, until time t(subscript 1) when the fuel is exhausted.

the equation for this is: position at that time=initial position+initial velocity times t(time)+0.5 times 3 times 9.81m/s^2 times T^2

i know initial velocity and position are zero, so all i got left over is the rest of the equation.

a=3g(g being accel. due to gravity) and T(subscript 1)=5.00s
it says to give ur answer in meters. i ended up with 368 meters. but it said that i forgot a numerical factor?
 
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[tex]x = \frac{1}{2} at^2 = \frac{1}{2} (3*9.8)(5)^2 = 367.5m[/tex]
 
thats what i basically entered but it keeps saying that I am off by a numerical factor? why the hell does it keep saying that.

the height I am supose to give is in this form H (subscript) 3= the answer.

it also says express the answer numerically in meters using g=9.81 m/s^2. just to be clear on that. i don't know what's the problem
 
I don't think this has to do with sig figs.

Compute the velocity at the time when all the fuel is burnt.From then on,the rocket goes straight up due to inertia.Gravity will be then the only force acting on it.

Your number ~368 is too small.

Daniel.
 
Are you trying to find the height when the fuel is burnt, or the final height? If its the first, then 368 is the answer.
 
it says to look for the maximum height
 
In that case find the velocity at t_1, then use the same equation you gave above with v_0 = v(t_1) and a = -9.8

Solve v_0 - at = 0 for a = 9.8 and v_0 = v(t1) to find where the velocity is 0 (the top). Use that value for t.

This is the distance traveled after the fuel is burned out.
 
Last edited:
how would i go about computing the velocity at T_1.?
 
  • #10
You underwent constnat acceleration of 3*9.8 for 5 seconds.
 
  • #11
thanks for the help. guys.

i have another quetion, but i don't know how to type these leters the right way

The next figure View Figure shows the velocity vectors corresponding to the upward motion of the power ball. Indicate whether its velocity and acceleration, respectively, are positive (upward), negative, or zero.
Use P, N, and Z for positive (upward), negative, and zero, respectively. Separate the letters for velocity and acceleration with a comma.

i tried typing in v p, a n, and other combnations but said it had the wrong number of terms separated by commas. how do i go about typing these terms in?


heres a the figure there referring to.
 

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  • #12
I think its looking for just p, n
Those are correct answers.
 
  • #13
thanks a lot man, that helped with the next problem. i really didnt know how to input these terms in.
 

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