Orbit

Physics: How To Get In and Out of Orbit

On my science blog, I shared my general thoughts on the wonderful movie Hidden Figures.  On this post, I want to answer the one question I've received the most - how do you even get something into orbit around the Earth? And how do you leave orbit entirely?

As with all of my posts, you can skip the diagrams if you want - the text should give you the general idea. Now on with the show!

Getting to Orbit

When we say a satellite is in orbit around the Earth, we mean that the satellite is traveling at the exact speed to counteract the force of gravity pulling it down. This means that the satellite is constantly falling, but its going fast enough so that it stays the same height above the Earth.  This results in the satellite traveling in a circular motion.  There are two forces acting on a satellite in this case:

  1. The centripetal force.  For circular motion to occur, this force must point inward toward the center of the circle
  2. The gravitational force.  This force exists between any two objects in our known galaxy.  It is directed between the centers of both objects (in this case, the satellite and the Earth)

For our satellite to stay in a circle, both of these forces must be the same.  This means that we can set the centripetal force equal to the gravitational force.  Solving this equation gives us a velocity of approximately 8 kilometers per second, or 17,682 miles per hour.  This is the speed that any satellite (including the International Space Station) has to achieve to be able to stay in orbit.  It's also why satellite launches tend to curve right after leaving the launchpad - they need to get to the orbital speed and be parallel to the Earth's surface so they can be pulled into circular obit.

Speed to Stay in Orbit.png

 

Leaving Orbit

My shirt has the answer!

My shirt has the answer!

What if we wanted to find the speed needed to leave orbit entirely?  This is what NASA did during our trips to the moon, and what NASA will do for our upcoming trips to Mars. The calculation is more complicated than getting to orbit, but we can find the speed needed by using a a familiar example of dropping a ball on the ground.

First, let's talk about energy. Total energy is expressed in two forms: kinetic energy (energy proportional to the speed of the ball) and potential energy (energy proportional to the distance above the surface). Before you drop a ball, it is motionless, so its kinetic energy is zero.  Right before the ball impacts the ground, it is right next to the surface, so its potential energy is zero.  

The total energy throughout this entire trip must remain the same, so we can set the the potential energy before dropping the ball equal to the kinetic energy right before it hits the ground. Solving this equation gives us a final velocity equal to the square root of 2 * times the acceleration due to gravity * the original height the ball was dropped from.  Note that just like with getting to orbit, the speed does not depend on the mass of the ball. 

 

The same energy situation applies if we throw a ball upwards, but our initial and final conditions are different.  Now, we want to look at the energy of the ball just before it leaves the orbit of the Earth and compare it to the energy of the ball when it is an infinite distance off, when Earth's gravity diminishes to negligible value and the ball has zero energy.  The reason we look at an infinite distance is because the force of gravity diminishes as you get farther from something, but never quite gets to zero. 

Just like in the case of the dropped ball, we can set the potential and kinetic energy at the beginning (when the ball leaves orbit) equal to the energy when the ball stops.  We can then solve for the escape velocity, which comes out to be very similar to the speed of the dropped ball!  Solving this equation gives us a velocity of 11.2 kilometers per second, or 25,000 miles per hour.

Orbit - Speed of a Thrown Ball Upwards.png