| CPC G08G 5/76 (2025.01) [G01S 13/953 (2013.01)] | 18 Claims |

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1. An aircraft antenna element comprising:
an aircraft antenna;
an antenna housing;
an atmospheric gas sensor suite; and
at least one processor connected to a memory for embodying processor executable code,
wherein:
the antennas housing defines an air inlet;
the air inlet is in fluid communication with the atmospheric gas sensor suite; and
the processor executable code configures the at least one processor to:
receive sensor data from the atmospheric gas sensor suite;
produce a contrail dissipation prediction based on the sensor data;
establish a data connection via the aircraft antenna; and
transmit the atmospheric gas sensor data to a network via the data connection.
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