Aircraft having a magnetically couplable payload module

An aircraft configured for thrust-borne lift in a vertical takeoff and landing flight mode and wing-borne lift in a forward flight mode, the aircraft comprising:

• an airframe having first and second wings with first and second pylons extending therebetween, the first and second pylons each having a payload station;
• a distributed propulsion system coupled to the airframe, the distributed propulsion system including at least two propulsion assemblies coupled to the first wing and at least two propulsion assemblies coupled to the second wing, the propulsion assemblies configured to provide vertical thrust in the vertical takeoff and landing flight mode and forward thrust in the forward flight mode;
• a control system operably associated with the distributed propulsion system and operable to independently control each of the propulsion assemblies;
• and
• a payload module configured to be transported by the airframe from a pickup location to a delivery location;
• wherein, the payload module is magnetically coupled between the payload stations of the first and second pylons during transportation;
• wherein, responsive to a command from the control system, the payload module is magnetically decoupled from the payload stations at the delivery location;
• wherein, in the vertical takeoff and landing flight mode, the first wing is forward of the payload module and the second wing is aft of the payload module;
• and
• wherein, in the forward flight mode, the first wing is below the payload module and the second wing is above the payload module forming a biplane configuration.