Electric brake system with flexible force transfer member

A aircraft brake system comprising

• an aircraft brake disk mounted proximate to a first portion of a strut;
• an aircraft brake head;
• a plurality of rams mounted on the aircraft brake head positioned to apply braking force to the aircraft brake disk,
• an electric motor for actuating the plurality of rams, the electric motor mounted directly on a landing gear well proximate to a second portion of the strut, the first portion of the strut opposite the second portion of the strut when the strut is in a deployed position;
• a gearbox comprising a plurality of gears to reduce an input force, wherein the gearbox distributes force equally between each of the plurality of rams, wherein the gearbox transfers a first force from the gearbox directly to a first ram in the plurality of rams;
• a first cable connecting the electric motor to the gearbox for transferring the input force from the electric motor to the gearbox, and
• a plurality of secondary cables for transferring force from the gearbox to each ram in the plurality of rams other than the first ram, the plurality of secondary cables connecting the gearbox to each ram in the plurality of rams other than the first ram.