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At space agencies worldwide, in university labs, and at start-up companies, nuclear fusion propulsion is on the agenda. In the United States, Congress approved USD 125 million in funding in May for the development of nuclear propulsion rockets and called upon NASA "to develop a multi-year plan that enables a " from both fission and fusion. The Russian space agency Roscosmos is working on a "" in collaboration with the Kurchatov Institute¡ªa project "made possible by advances made in the study of plasma fusion processes. The Advanced Concept Team at the European Space Agency (ESA), in collaboration with European universities, is conducting a study on the feasibility of . And China intends to develop of nuclear carrier rockets by the mid-2040s (without specifying whether they will be fission or fusion-propelled).

 

Rockets lift from their launchpad and vessels are propelled through deep space by the simple principle of action and reaction: heated exhaust gas is expelled at high speed through a nozzle and, in reaction, a thrust force is exerted on the vessel.

 

Conventional rockets are propelled by chemical combustion, which requires considerable amounts of ¡ªliquid hydrogen and liquid oxygen, or kerosene-like propellant¡ªthat are ignited at different stages of the ascent into space.

 

 

Propelling rockets by atomic bombs, detonated at very short intervals at the rear end of a rocket, was at one point contemplated. From 1958 to 1963 Project Orion, funded by the US Advanced Research Projects Agency (ARPA, today DARPA), the US Air Force, the Atomic Energy Commission and to a lesser extent NASA, aimed at precisely that.

 

The ban on atmospheric nuclear tests in 1963 put an end to the project. Five years later however, in a Physics Today article titled "," Project Orion's chief scientist Freeman Dyson suggested that "deuterium fusion explosions" would provide even more thrust and velocity to the bomb-powered rocket and spaceship.

 

Fifty years later, fusion is still a serious contender for space propulsion although not in its "explosive" applications. Fusion reactors are now contemplated as a heat source that would bring propellant to extremely high temperature (and hence high-velocity exhaust), or expel ultra-hot plasma to provide thrust.

 

Depending on the concept, the exhaust velocity of a fusion-propelled rocket would be in the range of 150-350 kilometres per second. Planet Mars could be reached  or even less, as compared to eight months with a conventional propulsion system. The intriguing moons of Jupiter and Saturn would be reachable in reasonable time and the way to exoplanets would open for exploration.

 

Using the power of fusion to propel rockets to speeds otherwise unattainable, and hence dramatically shortening the duration of space travel, may sound like the stuff of science fiction. And literally, it is: in the 2014 blockbuster Interstellar, the spaceship that carries passengers on a quest for inhabitable planets is fuelled by "compact tokamaks" which also provide the vessel's electricity.

 

 

A fusion reactor, however, is not necessarily a tokamak.

 

A NASA-funded joint venture between the University of Washington in Seattle and a small company named MSNW LLC focused on the development of advanced space propulsion systems has developed a small field-reversed pulsed-fusion device  (akin to the concept of 1980s-1990s) to be extrapolated into a "fusion drive engine." Promoters of the project say that they are at work  of "a fusion-powered rocket aimed to clear many of the hurdles that block deep space travel, including long times in transit, exorbitant costs and health risks."

 

In a similar move, the Princeton Plasma Physics Laboratory (PPPL) has entered into a with a company called Princeton Satellite Systems to work on a  engine for space exploration. Two years ago, NASA a half-a-million dollar grant to the venture, which was also by a US Federal Laboratory Consortium award in October last year.

 

In the projected direct fusion drive engine, fusion power would not be produced by the deuterium/tritium (DT) reactions of °ÄÃÅÁùºÏ²Ê¸ßÊÖ or future electricity-generating plants. While the DT reaction is the most accessible in today's state of technology, it has two significant drawbacks, particularly for manned space exploration. Tritium is a radioactive element, and the fusion reactions produce a flux of highly energetic neutrons from which humans and electronic equipment must be heavily shielded.

 

The deuterium/helium-3 reaction that is planned for the direct fusion drive engine has neither of these limitations: both elements are stable and so are the reaction products, hydrogen and helium. As the reaction is "," no heavy shielding would be required for protection.

 

There is, however, one big catch: the temperature required to fuse deuterium and helium-3 nuclei is about ten times higher than that required for DT fusion and no device has yet achieved this level of energy. (The present record is held by the Japanese tokamak JT-60U, which reached an ion temperature of half-a-billion degrees.)

 

The developers of the direct fusion drive claim that their engine could be operational , which might appear to be a wildly optimistic projection. It might take decades before fusion propulsion quits the realm of science fiction and enters the reality of space travel.

 

But among space-faring nations there is now a consensus, which the Department of Aeronautics and Astronautics at Washington University, one of the top aerospace schools in the United States, has : "Fusion energy is, in principle, the only conceivable source of energy for rapid, efficient, rocket space travel to Mars, the outer planets, and nearby stars."