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See also: Project Daedalus, a British study of interstellar spacecraft design.
It starts from the original 1970s Project Daedalus study conducted by members of the British Interplanetary Society.
It has been suggested that the restrictions of the Treaty would not apply to the Project Daedalus fusion microexplosion rocket.
The main alternative to magnetic confinement is inertial confinement fusion, such as that proposed by Project Daedalus.
A quantitative engineering analysis of a self-replicating variation on Project Daedalus was published in 1980 by Robert Freitas.
Project Daedalus was to be a robotic interstellar probe to Barnard's Star that would travel at 12% of the speed of light.
Project Daedalus was a study conducted between 1973 and 1978 by the British Interplanetary Society to design a plausible unmanned interstellar spacecraft.
Project Daedalus later proposed fusion explosives (deuterium or tritium pellets) detonated by electron beam inertial confinement.
Built and launched in Jovian orbit, it would reach Barnard's Star in 47 years under parameters similar to those of the original Project Daedalus.
He is the leading author of the report on the Project Daedalus interstellar, fusion powered starship concept, published by the British Interplanetary Society.
The British Interplanetary Society's hypothetical Project Daedalus interstellar probe design was fueled by helium-3 mines in the atmosphere of Jupiter, for example.
Newer designs using inertial confinement fusion have been the baseline for most post-Orion designs, including Project Daedalus and Project Longshot.
Friedwardt Winterberg described how rocket engines incorporating fusion micro-explosions could provide enough acceleration to convey a large mass in a reasonable amount of time, a concept derived from Project Daedalus.
The British Interplanetary Society promotes ideas for the exploration and utilization of space, including a Mars colony, future propulsion systems (see Project Daedalus), terraforming, and locating other habitable worlds.
The first quantitative engineering analysis of such a spacecraft was published in 1980 by Robert Freitas, in which the non-replicating Project Daedalus design was modified to include all subsystems necessary for self-replication.
Project Daedalus (1973-1978) Project Daedalus was a proposed nuclear pulse propulsion craft that used inertial confinement fusion of small pellets within a magnetic field nozzle to provide motive force.
Nuclear pulse propulsion might enable such interstellar travel with a trip timescale of a century, beginning within the next century, inspiring several studies such as Project Orion, Project Daedalus, and Project Longshot.
Reaction Engines was founded in 1989 by Alan Bond (lead engineer on the British Interplanetary Society's Project Daedalus) and Richard Varvill and John Scott-Scott (the two principal Rolls-Royce engineers from the RB545 engine project).
In the 1970s the Nuclear Pulse Propulsion concept further was refined by Project Daedalus by use of externally triggered inertial confinement fusion, in this case producing fusion explosions via compressing fusion fuel pellets with high-powered electron beams.
According to his faculty webpage, In 1954 he "made the first proposal to test general relativity with atomic clocks in earth satellites" and his thermonuclear microexplosion ignition concept was adopted by the British Interplanetary Society for their Project Daedalus Starship Study.
The possibility of using interstellar messenger probes for interstellar communication - known as Bracewell probes - was first suggested by Ronald N. Bracewell in 1960, and the technical feasibility of this approach was demonstrated by the British Interplanetary Society's starship study Project Daedalus in 1978.
Alan Bond (born 1944 in Ripley, Derbyshire) is Managing Director of Reaction Engines Ltd and associated with Project Daedalus, Blue Streak missile, HOTOL, Reaction Engines Skylon and the Reaction Engines A2 hypersonic passenger aircraft.
Alternately the antimatter-fusion hybrid drive the Valkyrie uses to accelerate up to 0.2 c would require much less antimatter and, with an exhaust velocity of 30-60,000 km s, still compares quite favorably with competing engines such as the inertial confinement pulse drive used by Project Daedalus or Project Orion (nuclear propulsion).