“…The idea of using fusion power for spacecraft propulsion has a long history [11][12][13][14], with its support arising from the high energy density of the fuel and the high velocity of the fusion products. Early proponents of fusion rockets that provided steady propulsion based their designs on the fusion devices that are tokamaks [15,16], mirror machines [17] and levitated dipoles [18]. The experimental results of the early period in fusion history indicated that the plasma's anomalous transport, meaning poor plasma energy confinement, Deuterium-Tritium (D-T) burning, large and powerful machines, many meters in diameter, producing over a gigawatt in power and requiring a meter or more of neutron shielding.…”