Aircraft Design Calculator

The “Mass of Elevators” in aircraft design refers to the total mass of the movable control surfaces known as elevators. Elevators are located on the tail (horizontal stabilizer) of an aircraft and are used to control the aircraft’s pitch or nose-up and nose-down movement. Here’s the formula, definition, and SI unit for the Mass of […]

The “Mass of Control Surfaces” in aircraft design refers to the total mass of the movable surfaces on an aircraft that are used to control its movement and attitude during flight. These control surfaces include ailerons, elevators, and rudders, among others. Here’s the formula, definition, and SI unit for the Mass of Control Surfaces: Formula

The “Mass of Control System” in aircraft design refers to the total mass of the components that make up the aircraft’s control system. The control system includes various elements such as control surfaces, control cables, rods, linkages, and actuating mechanisms that are used to control the aircraft’s movement and attitude during flight. Here’s the formula,

The “Mass of Fuel Tank” in aircraft design refers to the total mass of the fuel tank or tanks installed in an aircraft. Fuel tanks are integral components of an aircraft’s design, and they hold the fuel needed for propulsion during flight. Here’s the formula, definition, and SI unit for the Mass of Fuel Tank:

The “Mass of Ribs” in aircraft design refers to the total mass of the wing ribs, which are structural components that give the wing its airfoil shape and provide support to the wing’s skin or covering. Ribs are typically spaced along the wing’s span to maintain its shape and structural integrity. Here’s the formula, definition,

The “Mass of Wing Structure” in aircraft design refers to the total mass of the structural components that make up the wings of an aircraft. These components include the wing’s spars, ribs, skin, fuel tanks (if integrated into the wings), and other structural elements. Here’s the formula, definition, and SI unit for the Mass of

The “Mass of Other Brake Components” in aircraft design refers to the total mass of various additional components that are part of the aircraft’s braking system but not included in the categories of brake pads, brake discs, or brake calipers. These components can include items such as hydraulic lines, valves, sensors, and other associated hardware.

The “Mass of Brake Calipers” in aircraft design refers to the total mass of the brake calipers used in the aircraft’s braking system. Brake calipers are essential components that hold the brake pads and facilitate their movement when engaged. Here’s the formula, definition, and SI unit for the Mass of Brake Calipers: Formula for Mass

The “Mass of Brake Pads” in aircraft design refers to the total mass of the brake pads used in the aircraft’s braking system. Brake pads are essential components that press against the brake discs or rotors to generate friction and deceleration during landing and ground operations. Here’s the formula, definition, and SI unit for the

The “Mass of Brake Discs” in aircraft design refers to the total mass of the brake discs or rotors used in the aircraft’s braking system. These brake discs are essential components for generating friction and deceleration during landing and ground operations. Here’s the formula, definition, and SI unit for the Mass of Brake Discs: Formula