Showing posts with label specific impulse. Show all posts
Showing posts with label specific impulse. Show all posts

Wednesday, September 2, 2015

Specific impulse

Our topic for today is another rocketry concept: Specific impulse (usually abbreviated Isp).  Basically, it's how efficient your rocket engine is.  It's defined by how far each unit of fuel moves your rocket.
Here's the formula:
Isp equation  Where:
  • I_{{sp}} is the specific impulse in meters per second
  • F_{T} the thrust in newtons
  • {\dot  m} the fuel consumption in kg/s
So, Isp is how much thrust you get per unit of fuel.

If your Isp is higher, then you can get more Delta-V with the same rocket.  In the rocket equation, v_\text{e} is used instead of Isp, but the concepts are the same.