An aircraft , comprising: a passenger cabin configured to transport one or more passengers; a battery pack configured to power one or more electronic components of the aircraft ; and a cabin thermal management system configured to regulate a cabin temperature of the passenger cabin by transferring thermal energy from the battery pack to the passenger cabin , wherein the cabin thermal management system further comprises a valve coupled to a thermal loop , a heat exchanger coupled to the thermal loop , disposed in or proximate to the passenger cabin and configured to transfer the thermal energy between the battery pack and the passenger cabin ; wherein the cabin thermal management system is configured to receive a user input that the passenger cabin is to be cooled ; wherein the thermal loop is coupled to one or more channels of the battery pack , wherein the thermal loop is configured to allow fluid from the one or more channels to circulate therein; and wherein the valve is configured to divert the fluid toward the heat exchanger if a first temperature measurement by a battery temperature sensor is lower than a first temperature measurement by a cabin temperature sensor , wherein the valve is configured to divert the fluid away from the heat exchanger if a second temperature measurement by the battery temperature sensor is higher than or equal to a second temperature measurement by the cabin temperature sensor , and wherein the cabin thermal management system further comprises a supplemental heating, ventilation, and air conditioning system configured to cool the passenger cabin if the second temperature measurement by the battery temperature sensor is higher than or equal to the second temperature measurement by the cabin temperature sensor . a passenger cabin configured to transport one or more passengers; a battery pack configured to power one or more electronic components of the aircraft ; and a cabin thermal management system configured to regulate a cabin temperature of the passenger cabin by transferring thermal energy from the battery pack to the passenger cabin , wherein the cabin thermal management system further comprises a valve coupled to a thermal loop , a heat exchanger coupled to the thermal loop , disposed in or proximate to the passenger cabin and configured to transfer the thermal energy between the battery pack and the passenger cabin ; wherein the cabin thermal management system is configured to receive a user input that the passenger cabin is to be cooled ; wherein the thermal loop is coupled to one or more channels of the battery pack , wherein the thermal loop is configured to allow fluid from the one or more channels to circulate therein; and wherein the valve is configured to divert the fluid toward the heat exchanger if a first temperature measurement by a battery temperature sensor is lower than a first temperature measurement by a cabin temperature sensor , wherein the valve is configured to divert the fluid away from the heat exchanger if a second temperature measurement by the battery temperature sensor is higher than or equal to a second temperature measurement by the cabin temperature sensor , and wherein the cabin thermal management system further comprises a supplemental heating, ventilation, and air conditioning system configured to cool the passenger cabin if the second temperature measurement by the battery temperature sensor is higher than or equal to the second temperature measurement by the cabin temperature sensor . <EOS>