Spaceship propulsion by momentum transfer

Abstract

A propulsion system for spaceships wherein a first electromagnetic projectile launcher (EMPL) accelerates "smart" projectiles into space and on appropriate trajectories to rendezvous with a distant spaceship at some later time. The smart projectiles stabilize themselves in space using a system of on board thrusters operated by computers. Laser beams and radio transmissions are directed at the spaceship and are monitored by sensors aboard the spaceship. Computers on board the spaceship determine any necessary course corrections for the projectiles based upon the spaceship's sensor system. Appropriate commands are radioed to the projectiles which execute the commanded maneuvers to alter their trajectories. The spaceship carries a second EMPL and a nuclear-powered electricity generating facility to provide electricity to operate the EMPL. The spaceship, the second EMPL and the nuclear power facility are all rotated axially about the long axis of the EMPL to provide both gyroscopic stabilization and also artifical gravity for the crew of the spaceship. The second EMPL is used to catch the projectiles which transfers the momentum of the projectiles to the spaceship thereby accelerating it in the desired direction. Additional acceleration of the spaceship is achieved by again launching the captured projectiles in a direction opposite to the desired direction of motion of the spaceship. The spaceship can be decelerated in a similar manner. Mars can be reached in two months using this system.

Dependencies are inferred from the claim text.