Calculating Energy Required for Space Shuttle Orbit Boost

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Homework Help Overview

The problem involves calculating the energy required for a space shuttle to transition from a 250 km high circular orbit to a 610 km high circular orbit. The shuttle's mass is given, and participants are discussing the energy calculations involved in this orbital change.

Discussion Character

  • Exploratory, Conceptual clarification, Mathematical reasoning

Approaches and Questions Raised

  • Participants are examining the potential and kinetic energy components involved in the energy calculations. There is a focus on the correct formulation of gravitational potential energy and the inclusion of kinetic energy in the total mechanical energy.

Discussion Status

Some participants are questioning the original calculations and suggesting that the kinetic energy has been overlooked. Others are providing alternative formulations for potential energy and discussing the implications of these changes on the overall energy required for the orbital boost.

Contextual Notes

There appears to be a discrepancy between the calculated energy and the value provided in the textbook, leading to further exploration of the assumptions and equations used in the calculations.

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Homework Statement


The space shuttle is in a 250 km high circular orbit. It needs to reach a 610 km high circular orbit to catch the Hubble telescope for repairs. The shuttle's mass is 75000 kg. How much energy is required to boost it to the new orbit?


Homework Equations





The Attempt at a Solution



I keep coming up with answer that is twice the answer in the back of my book

Uf= E + Ui
(-6.67E-11)(5.98E24kg)(75000kg)/(610000m+6.37E6) = E + (-6.67E-11)(5.98E24)(75000kg)/(250000m+6.37E6)

E= 2.33E11 J


book gives 1.17E11
 
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You are ignoring kinetic energy.
 
bcjochim07 said:

Homework Statement


The space shuttle is in a 250 km high circular orbit. It needs to reach a 610 km high circular orbit to catch the Hubble telescope for repairs. The shuttle's mass is 75000 kg. How much energy is required to boost it to the new orbit?


Homework Equations





The Attempt at a Solution



I keep coming up with answer that is twice the answer in the back of my book

Uf= E + Ui
(-6.67E-11)(5.98E24kg)(75000kg)/(610000m+6.37E6) = E + (-6.67E-11)(5.98E24)(75000kg)/(250000m+6.37E6)

E= 2.33E11 J


book gives 1.17E11

In Uf= E + Ui,
Ui should be the sum of kinetic energy mv^2/2 and potential energy -GmM/r
using GmM/r^2 = mv^2/r, we can get mv^2/2 = GmM/(2r)
so U = -GmM/(2r), not -GmM/r as you used.
then we can get the half of your answer.
 
I know for a fact that this solution is correct:

We are looking for the change in mechanical energy.

Emech = (1/2)Ug
Therefore, ∆Emech = (1/2)∆Ug

G = 6.67 X 10^-11
Me = 5.98 X 10^24 kg
Ms = 7.5 X 10^4 kg
Re = 6.37 X 10^6 m
r1 = Re + 2.5 X 10^5 m
r2 = Re + 6.1 X 10^5 m

Solve for Ug at r1. (Call this Ug1)
Ug1 = (-G(Me)(Ms))/(r1) = -4.519 X 10^12 J

Solve for Ug at r2. (Call this Ug2)
Ug2 = (-G(Me)(Ms))/(r2) = -4.286 X 10^12 J

∆Ug = Ug2 - Ug1 = 2.33 X 10^11 J

∆Emech = (1/2)∆Ug = 1.17 X 10^11 J
 
Last edited:

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