CABIN THERMAL MANAGEMENT SYSTEM

Various implementations directed to a cabin thermal management system (220) are provided. In one implementation, an aircraft (100, 200) may include a passenger cabin (105, 205) configured to transport one or more passengers. The aircraft (100, 200) may also include a battery pack (110, 210) configured to power one or more electronic components of the aircraft. The aircraft (200) may further include a cabin thermal management system (220) configured to regulate a cabin temperature of the passenger cabin (205) by transferring thermal energy from the battery pack (210) to the passenger cabin (205).