A spacecraft requires a continuous electric power of 1MW for a 100-day mission. Its fusion reactor operates at 25% efficiency and uses the deuterium–tritium reaction that releases 17.6MeV per fusion event. The number of fusion events needed for the mission is approximately
(a) 3.1×1024
(b) 6.1×1024
(c) 1.2×1025
(d) 5.9×1025