Mass in a satellite changes orbit

Click For Summary
SUMMARY

The discussion centers on the mechanics of moving a mass in a satellite to achieve a higher orbit. It establishes that energy must be added to the system, specifically through a one-time impulse, which alters the orbit into an elliptical path rather than a true higher circular orbit. The key equations referenced include the potential energy equation, E_p=\frac{GMm}{r}, and the gravitational force equation, F=\frac{GMm}{r^2}. The conclusion emphasizes the necessity of changing the velocity direction to achieve the desired orbital trajectory.

PREREQUISITES
  • Understanding of gravitational potential energy and its equation
  • Familiarity with gravitational force and its equation
  • Basic knowledge of orbital mechanics
  • Concept of impulse and its effect on satellite motion
NEXT STEPS
  • Research Hohmann Transfer Orbits for efficient orbital transfers
  • Study the principles of impulse and its application in orbital mechanics
  • Explore the effects of elliptical orbits on satellite trajectories
  • Learn about energy conservation in orbital maneuvers
USEFUL FOR

Aerospace engineers, physics students, and anyone involved in satellite operations or orbital mechanics will benefit from this discussion.

Karol
Messages
1,380
Reaction score
22

Homework Statement


A i kg mass is in a satellite must move to a higher orbit. energy must be added.
Can this energy be added at one time, by shooting the mass?

Homework Equations


Potential energy: ##E_p=\frac{GMm}{r}##
Gravitational force: ##F=\frac{GMm}{r^2}##

The Attempt at a Solution


The velocity at the higher circular orbit is lower but the potential energy much higher so energy must be added. but if i shoot the mass it reaches the higher orbit with the correct, lower energy but the direction isn't correct, i must change the velocity direction to tangent to earth, right?
 
Physics news on Phys.org
You are basically correct. A one time impulse will change the satellite's orbit into an ellipse that will continue to revisit the same height as the starting point. This doesn't really count as a "higher orbit".

You might find investigating Hohmann Transfer Orbits will give you insight into the problem and its solution.
 

Similar threads

  • · Replies 30 ·
2
Replies
30
Views
2K
  • · Replies 1 ·
Replies
1
Views
2K
Replies
5
Views
3K
Replies
5
Views
2K
  • · Replies 3 ·
Replies
3
Views
3K
  • · Replies 14 ·
Replies
14
Views
3K
  • · Replies 3 ·
Replies
3
Views
2K
Replies
1
Views
2K
Replies
1
Views
2K
  • · Replies 7 ·
Replies
7
Views
2K