Forces and Motion

 

Orbital

Velocity

Equation

 

     v = (GM/r)½

1.15

 

Escape

Velocity

Equation

 

     v = (2GM/r)½

1.16

Orbital Motion

Notes

• A satellite’s orbit is defined by the force of gravity and tangential velocity.

 

• All objects orbit in elliptical orbits

 

• Objects sweep out equal areas in equal time

 

• P2 ~ a3

 

• Orbiting objects are continually falling toward their central body.

 

 

Notebook

© 2013 by Wheeling Jesuit University/Center for Educational Technologies®. 316 Washington Ave., Wheeling, WV 26003-6243. All rights reserved. Privacy Policy and Terms of Use.