Calculating Energy Required for Space Shuttle Orbit Boost

  • Thread starter Thread starter bcjochim07
  • Start date Start date
  • Tags Tags
    Energy Space
Click For Summary
SUMMARY

The energy required to boost the Space Shuttle from a 250 km orbit to a 610 km orbit is calculated to be 1.17 x 1011 J. This calculation incorporates both potential and kinetic energy, utilizing the gravitational constant G = 6.67 x 10-11 N(m/kg)2 and the mass of the Earth Me = 5.98 x 1024 kg. The initial potential energy at the lower orbit (Ug1) is -4.519 x 1012 J, while the potential energy at the higher orbit (Ug2) is -4.286 x 1012 J, leading to a change in mechanical energy (∆Emech) of 1.17 x 1011 J.

PREREQUISITES
  • Understanding of gravitational potential energy and kinetic energy equations
  • Familiarity with the gravitational constant (G = 6.67 x 10-11 N(m/kg)2)
  • Knowledge of mass and radius in orbital mechanics
  • Ability to perform calculations involving large numbers and scientific notation
NEXT STEPS
  • Study the derivation of gravitational potential energy equations in orbital mechanics
  • Learn about the principles of energy conservation in space travel
  • Explore the effects of altitude on orbital velocity and energy requirements
  • Investigate the mechanics of the Space Shuttle and its propulsion systems
USEFUL FOR

Aerospace engineers, physics students, and anyone involved in space mission planning or orbital mechanics will benefit from this discussion.

bcjochim07
Messages
366
Reaction score
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
 
Physics news on Phys.org
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:

Similar threads

  • · Replies 1 ·
Replies
1
Views
3K
  • · Replies 4 ·
Replies
4
Views
2K
Replies
5
Views
3K
  • · Replies 27 ·
Replies
27
Views
4K
  • · Replies 1 ·
Replies
1
Views
3K
  • · Replies 38 ·
2
Replies
38
Views
5K
  • · Replies 2 ·
Replies
2
Views
6K
  • · Replies 6 ·
Replies
6
Views
10K
  • · Replies 1 ·
Replies
1
Views
2K
Replies
37
Views
3K