Abstract
A power system for an aircraft includes at least one gas turbine engine arranged to burn a fuel so as to provide power to the aircraft; at least one first fuel tank arranged to be used to power ground-based operation of the aircraft; at least one secondary fuel tank arranged to contain a fuel to be used to power the aircraft in flight; and a fuel manager arranged to control fuel supply so as to take fuel from only the at least one first fuel tank to power at least the majority of ground-based operations.