AIRCRAFT BRAKE TEMPERATURE CONTROL SYSTEM

An aircraft brake temperature control system (BTCS) for controlling a temperature of a brake of a landing gear of the aircraft . The BTCS includes a controller configured to cause a thermal management system to regulate the temperature of the brake , on the basis of a selection of an objective for regulating the temperature of brake from a plurality of objectives for regulating the temperature of the brake. An aircraft includes the BTCS; and a method controls a temperature of a brake of a landing gear of an aircraft.