“…The shield thickness of a D-3 He TR is assumed as 0.7 m, as in ARIES-3 [7]. Since 3 He gas is a very rare terrestrial resource, we assumed a scenario in which 3 He is transported from the lunar surface and estimated its cost as 200 US$/g [8]. …”
Social acceptance of fusion reactors depends largely on their economic viability. To investigate this issue, we estimate and compare the cost of electricity (COE) among D-T, D-3 He, and D-D fusion reactors. Three types of confinement systems are evaluated: the tokamak reactor (TR), the spherical tokamak reactor (STR), and helical reactor (HR). For each reactor type, COE parameter surveys are performed and new scaling laws for COE are derived. The COE for D-3 He and D-D is high and depends more strongly on plasma beta value and maximum magnetic field strength than that of D-T.
“…The shield thickness of a D-3 He TR is assumed as 0.7 m, as in ARIES-3 [7]. Since 3 He gas is a very rare terrestrial resource, we assumed a scenario in which 3 He is transported from the lunar surface and estimated its cost as 200 US$/g [8]. …”
Social acceptance of fusion reactors depends largely on their economic viability. To investigate this issue, we estimate and compare the cost of electricity (COE) among D-T, D-3 He, and D-D fusion reactors. Three types of confinement systems are evaluated: the tokamak reactor (TR), the spherical tokamak reactor (STR), and helical reactor (HR). For each reactor type, COE parameter surveys are performed and new scaling laws for COE are derived. The COE for D-3 He and D-D is high and depends more strongly on plasma beta value and maximum magnetic field strength than that of D-T.
“…However, 3 He gas is a very rare resource on the earth. In this study, we assumed a scenario in which 3 He is taken from the moon's surface [4]; the cost of 3 The electron and ion temperatures are assumed to be equal. Parabolic plasma temperature and density profiles are assumed:…”
“…By this time, with MTF providing the means for human exploration of the outer solar system, thriving transport, manufacturing and resource extraction infrastructure should be in place both at the Earth's Lagrange points and on the lunar surface. The process of helium-3 extraction from lunar regolith has already been seriously studied, with encouraging results (Wittenberg, 1992).…”
Abstract. Engineering details are presented for a magnetized target fusion (MTF) propulsion system designed to support crewed missions to the outer solar system. Basic operation of an MTF propulsion system is introduced. Structural, thermal, radiation-management and electrical design details are presented. The propellant storage and supply system design is also presented. A propulsion system mass estimate and associated performance figures are given. The advantages of helium-3 as a fusion fuel for an advanced MTF system are discussed.
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