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:

Where:
is the specific impulse in meters per second
the thrust in newtons
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,

is used instead of Isp, but the concepts are the same.