I really can't seem to wrap my head around why the specific impulse on a rocket is so much lower than that on a jet. I know a jet engine has a larger supply of oxygen, but I don't see why that has such a huge effect.
I also know exhaust velocity plays a large part, but I would have thought that...
Good point, I got confused, I was thinking of power = force*velocity, where it can be a part of the equation, the force is the resultant force, so it's the forward thrust minus the resistive force.
The way I see it, a constant supply of power, say from the engine in a car to its wheels, will cause it to accelerate at a decreasing rate because the kinetic energy the power supplies is proportional to the velocity squared. That makes sense because going faster will cause the car to encounter...