A gas turbine (100) of the present invention is a gas turbine which uses a hydrogen gas as a fuel, and comprises a combustor (20) which includes a fuel injection nozzle (23), and has a combustion chamber (24) in an interior of the combustor; a steam supply unit (40) which supplies steam to the combustor (20) to decrease a combustion temperature; and an air drier (50) which removes the steam from air to be supplied to the combustor (20) to dry the air.