2011
DOI: 10.1016/j.actaastro.2011.01.010
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Project Icarus: Optimisation of nuclear fusion propulsion for interstellar missions

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Cited by 23 publications
(8 citation statements)
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“…Freeland and Lamontagne 2015). Both approaches will continue to be aided by improved understanding of controlled nuclear fusion gained from experimental facilities designed to investigate the potential of fusion power on Earth, and continued refinement of the design concepts may be expected (Long 2016).…”
Section: Nuclear Rocketsmentioning
confidence: 99%
“…Freeland and Lamontagne 2015). Both approaches will continue to be aided by improved understanding of controlled nuclear fusion gained from experimental facilities designed to investigate the potential of fusion power on Earth, and continued refinement of the design concepts may be expected (Long 2016).…”
Section: Nuclear Rocketsmentioning
confidence: 99%
“…The Daedalus mission weight for Barnard's Star was about 53000 tonnes which may present orbital construction challenges in the nearfuture. Project Icarus proposed replacing the electron beam driver with laser and decreasing the nuclear pulse to 150 Hz with smaller pellets [25]. The fusion-driven rocket partially solves the problem by using metal liners to both contain the plasma and conversion to thrust [34].…”
Section: The Challenges Of Propulsionmentioning
confidence: 99%
“…Missions to neighboring star systems require high cruising speeds in order to reduce the total trip duration. There have been proposals based on fusion propulsion that aim to keep the total mission duration underneath 100 years [3], [13], which means that an average speed bigger than 0.0435 c is necessary in the case of Alpha Centauri [14]. The present analysis focuses on missions with the objective of performing scientific measurements in the target system, hence requiring orbital insertion around a star or a planet.…”
Section: Combination Of Msail and Esailmentioning
confidence: 99%
“…At the same time, there has to be some finite distance available for the acceleration and cruising phases, which are not part of the optimization and this was estimated equal to 1.5 light years. For that reason, the constraint was defined as in Equation 14:…”
Section: Optimization Processmentioning
confidence: 99%