I mean you still need to carry propellant: the stuff that is ablated away. It's just that the exhaust velocity is much higher.
Air from the atmosphere may be the propellant [1]. If sufficient velocity can be achieved before leaving the atmosphere, then no propellant is needed to be carried up on the way to orbit.
I can't find the video I saw, but here's a general link on the topic:
https://en.wikipedia.org/wiki/Laser_propulsion#Laser_energiz...
This comes with many problems, but it does bypass the rocket equation, while not requiring Project Orion levels of trouble.