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An aircraft includes a cooling compartment and an evaporative chiller configured to cool the cooling compartment. The evaporative chiller includes a compressor, an evaporator having airflow to the cooling compartment, and a condenser. The condenser has an exhaust airflow to cool the condenser. The e

An aircraft includes a cooling compartment and an evaporative chiller configured to cool the cooling compartment. The evaporative chiller includes a compressor, an evaporator having airflow to the cooling compartment, and a condenser. The condenser has an exhaust airflow to cool the condenser. The evaporative chiller has a condensate removal system removing condensate produced by the evaporator using the exhaust airflow of the condenser to discharge the condensate.

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1. An aircraft comprising: a cooling compartment; and an evaporative chiller configured to cool the cooling compartment, the evaporative chiller including a compressor, an evaporator configured to channel an airflow to the cooling compartment, and a condenser, the evaporative chiller having a conden

1. An aircraft comprising: a cooling compartment; and an evaporative chiller configured to cool the cooling compartment, the evaporative chiller including a compressor, an evaporator configured to channel an airflow to the cooling compartment, and a condenser, the evaporative chiller having a condenser air circuit configured to produce an exhaust airflow to cool the condenser, the evaporative chiller having a condensate removal system configured to remove condensate produced by the evaporator using the exhaust airflow to discharge the condensate, the condensate removal system being a plumbing-free condensate removal system, wherein the plumbing-free condensate removal system does not include plumbing pipes for the condensate extending away from and coming into the evaporative chiller. 2. The aircraft of claim 1, wherein the condensate removal system is configured to inject the condensate into the exhaust airflow. 3. The aircraft of claim 1, wherein the exhaust air with the condensate is discharged to a predetermined location within the aircraft. 4. The aircraft of claim 3, wherein the exhaust air with the condensate is discharged into a cabin of the aircraft. 5. The aircraft of claim 3, wherein the exhaust air with the condensate is discharged into a cargo compartment of the aircraft. 6. The aircraft of claim 1, wherein the evaporative chiller is at least one of coupled to and positioned in a galley of the aircraft having the cooling compartment. 7. The aircraft of claim 6, wherein the galley is a plumbing-free galley. 8. The aircraft of claim 1, wherein the evaporative chiller is separate from a galley of the aircraft in one of a crown of the aircraft or a cargo compartment of the aircraft. 9. The aircraft of claim 1, wherein the cooling compartment and the evaporative chiller are in a crown of the aircraft. 10. The aircraft of claim 1, wherein the cooling compartment and the evaporative chiller are in a cargo compartment of the aircraft. 11. The aircraft of claim 1, wherein the evaporative chiller includes an air supply duct in flow communication with the cooling compartment to deliver the airflow to the cooling compartment, the condenser air circuit for air cooling the condenser, the condenser air circuit having a condenser supply duct and a condenser exhaust duct, the condenser having a condenser fan configured to promote airflow through the condenser air circuit from the condenser supply duct to the condenser exhaust duct, the condensate removal system configured to inject the condensate into the condenser exhaust duct to be expelled with the exhaust airflow. 12. The aircraft of claim 1, wherein the condensate removal system includes an atomizer nozzle configured to inject the condensate into the exhaust airflow. 13. The aircraft of claim 1, wherein the condensate removal system includes a sponge configured to evaporate the condensate into the exhaust airflow of the condenser air circuit. 14. The aircraft of claim 1, wherein the condenser includes a condenser fan configured to create the exhaust airflow, the condenser fan having blades, the condensate removal system including a condensate collector configured to hold the condensate proximate to the fan, the blades being dipped in the condensate in the condensate collector and propelled away from the blades to inject the condensate into the exhaust airflow. 15. An aircraft comprising: a galley having a plurality of stowage compartments, at least one of the stowage compartments defining a cooling compartment, the galley being plumbing-free; an evaporative chiller coupled to the galley, the evaporative chiller configured to cool the cooling compartment, the evaporative chiller including a compressor at the galley, an evaporator at the galley configured to channel an airflow to the cooling compartment for cooling the cooling compartment, and a condenser at the galley, the evaporative chiller having a condenser air circuit configured to produce an exhaust airflow to cool the condenser; and a plumbing-free condensate removal system coupled to the plumbing-free galley, the plumbing-free condensate removal system including a condensate collector configured to collect condensate produced by the evaporator, the plumbing-free condensate removal system including a condensate re-ingestor configured to discharge the condensate into the exhaust airflow such that the condensate is configured to be discharged from the evaporative chiller, wherein the plumbing-free condensate removal system does not include plumbing pipes for the condensate extending away from and coming into the evaporative chiller. 16. The aircraft of claim 15, wherein the plumbing-free condensate removal system is configured to inject the condensate into the exhaust airflow. 17. The aircraft of claim 15, wherein the exhaust air with the condensate is discharged to at least one of a cabin of the aircraft and a cargo compartment of the aircraft. 18. The aircraft of claim 15, wherein the evaporative chiller includes an air supply duct in flow communication with the cooling compartment to deliver the airflow to the cooling compartment, the condenser air circuit for air cooling the condenser, the condenser air circuit having a condenser supply duct and a condenser exhaust duct, the condenser having a condenser fan configured to promote airflow through the condenser air circuit from the condenser supply duct to the condenser exhaust duct, the plumbing-free condensate removal system configured to inject the condensate into the condenser exhaust duct to be expelled with the exhaust airflow. 19. A galley comprising: a plurality of walls configured to extend between a crown and a floor of a cabin of an aircraft; a cooling compartment defined by the plurality of walls, the cooling compartment being configured to receive at least one of a galley cart and a stowage container; and an evaporative chiller coupled to at least one of the walls of the galley and configured to cool the cooling compartment, the evaporative chiller including a compressor, an evaporator configured to channel an airflow to the cooling compartment, and a condenser, the evaporative chiller having a condenser air circuit configured to produce an exhaust airflow to cool the condenser, the evaporative chiller having a plumbing-free condensate removal system configured to remove condensate produced by the evaporator using the exhaust airflow to discharge the condensate, wherein the plumbing-free condensate removal system does not include plumbing pipes for the condensate extending away from and coming into the evaporative chiller.