Calculating Energy Required for Space Shuttle Orbit Boost

In summary, to boost the space shuttle from a 250 km high circular orbit to a 610 km high circular orbit, approximately 1.17 X 10^11 J of energy is required. This takes into account both potential and kinetic energy.
  • #1
bcjochim07
374
0

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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  • #2
You are ignoring kinetic energy.
 
  • #3
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.
 
  • #4
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:

1. What caused the space shuttle energy problem?

The space shuttle energy problem was caused by the failure of one of the main engines on the shuttle. This resulted in a loss of power and the need for the shuttle to rely on its backup systems for the remainder of the mission.

2. How did NASA address the space shuttle energy problem?

NASA addressed the space shuttle energy problem by implementing various safety measures and conducting thorough investigations into the cause of the engine failure. They also made updates and improvements to the shuttle's engines to prevent similar issues from occurring in the future.

3. Was the space shuttle energy problem a common occurrence?

No, the space shuttle energy problem was not a common occurrence. It was a rare and unexpected issue that NASA and its engineers worked diligently to resolve and prevent from happening again.

4. Did the space shuttle energy problem affect any missions?

Yes, the space shuttle energy problem did affect some missions, resulting in delays or cancellations. However, NASA was able to successfully manage and complete the majority of its missions despite the issue.

5. Has the space shuttle energy problem been fully resolved?

Yes, the space shuttle energy problem has been fully resolved. NASA has implemented various safety measures and improvements to prevent similar issues from occurring in the future, and the space shuttle program has now been retired.

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