Yeah, but have you ever worked out the rocket equation for a spaceship that accelerates at 1G for a full year? There literally isn’t enough mass in our solar system, even with a ridiculous engine with an ISP of 5000 and perfect alchemy to convert all raw mass in the solar system to rocket fuel.
As far as I know Nuclear Thermal rockets have topped out around 1000. Project Orion is entirely theoretical and the ISP calculations should be taken with a grain of salt.