By using the concept of nuclear thermal rocket .
In a nuclear thermal rocket a working fluid, usually liquid hydrogen, is heated to a high temperature in a nuclear reactor, and then expands through a rocket nozzle to create thrust. In this kind of thermal rocket, the nuclear reactor's energy replaces the chemical energy of the propellant's reactive chemicals in a chemical rocket . If we can use thorium for this purpose it will be very cost effective for us .
But it is only possible if we are able to make a light weight thorium reactor which can provide required heat to liquid hydrogen .
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so basically its a chemical rocket without the oxidiser.. instead of oxidiser we are using nuclear heat here to produce high pressurised gas..
not very different from a chemical powered engine.. still u cant call it a nuclear propulsion .. it is nuclear powered propulsion..
ya this propulsion seems fast n strong as high pressurised gas will be released from nozzle generating trust. but the duration of propulsion will depend upon the amount of fuel it will carry. looks like cryogenic propulsion minus oxygen
but a propulsion where thrust is generated by forcing a volume of gas is not good for interstellar travel.. you have to carrry very very large amount of fuel.
contrarily in IOn engine.. a small amount of gas(inert) is kept in cylinder and each atom of gas is ionised.. which are realeased to generate small thrust but this thrust can be sustained for very long peroid of time with very little fuel.. here in this case u dnt have to carry large amount of fuel .. plus if you power such engines with nuclear reactor. its efficiency and thrust increases more.. once can travel more distance..