Abstract: An aircraft mission computing system includes an aircraft mission path computing engine, and a mission deck comprising a display and a display management assembly configured for displaying, on the display, at least one button for defining an operational specification of the mission. The computing engine is configured to be activated after defining the choice of operational specification using the definition button to determine at least one possible path of the aircraft based on the or each choice of defined operational specification using the or each definition button. The display management assembly is configured to display, on the display, after the activation of the computing engine, at least one outcome indicator providing mission feasibility information while respecting the or each operational specification choice.

Abstract: A cabin module deployable inside a vehicle so as to form at least a portion of an interior of the vehicle. The cabin module comprises a main body and a plurality of external walls. One or more of the plurality of external walls are moveable with respect to the main body. The module has a closed configuration for storage outside the vehicle, in which the plurality of external walls define at least a part of a first form factor of the module. The module has an open configuration for operational deployment in the vehicle, in which the plurality of external walls define at least a part of a second form factor of the module. The cabin module is reversibly changeable between the closed configuration and the open configuration by movement of the one or more external walls. The first form factor is different from the second form factor.

Abstract: An aircraft mission computing system includes an aircraft mission path computing engine, and a mission deck comprising a display and a display management assembly configured for displaying, on the display, at least one button for defining an operational specification of the mission. The computing engine is configured to be activated after defining the choice of operational specification using the definition button to determine at least one possible path of the aircraft based on the or each choice of defined operational specification using the or each definition button. The display management assembly is configured to display, on the display, after the activation of the computing engine, at least one outcome indicator providing mission feasibility information while respecting the or each operational specification choice.