A laser fusion rocket for interplanetary propulsion
- Paper ID
IAF-83-396
- author
- company
Lawrence Livermore National Laboratory
- country
U.S.A.
- year
1983
- abstract
A rocket powered by fusion microexplosions is well suited for quick interplanetary travel. Fusion pellets are sequentially injected into a magnetic thrust chamber. There, focused energy from a fusion “Driver” is used to implode and ignite them. Upon exploding, the plasma debris expands into the surrounding magnetic field and is redirected by it, producing thrust. This paper discusses the desired features and operation of the fusion pellet, its Driver, and magnetic thrust chamber. A rocket design is presented which uses slightly tritium-enriched deuterium as the fusion fuel, a high temperature KrF* laser as the Driver, and a thrust chamber consisting of a single superconducting current loop protected from the pellet by a radiation shield. This rocket can be operated with a power-to-mass ratio of 110 IF gm*1, which permits missions ranging from occasional 9 day “VIP" service to Mars, to routine 1 year, 1500 ton, Plutonian cargo runs.