The “Mass of Main Landing Gear” in aircraft design refers to the total mass of the landing gear components specifically located under the aircraft’s main wings. This includes items such as the wheels, struts, brakes, tires, and associated structural elements for the main landing gear. Here’s the formula, definition, and SI unit for the Mass of Main Landing Gear:
Formula for Mass of Main Landing Gear: The Mass of Main Landing Gear is determined by adding the masses of all components related to the main landing gear. Mathematically, it can be expressed as:
- Mass of Main Landing Gear: The total mass of all components associated with the main landing gear, typically measured in kilograms (kg) or pounds (lb).
- Mass of Main Wheels: The mass of the main landing gear wheels.
- Mass of Main Landing Gear Struts: The mass of the struts that support the main landing gear and provide shock absorption during landing.
- Mass of Main Brakes: The mass of the aircraft’s main braking system components.Mass of Main Tires: The mass of the tires mounted on the main landing gear wheels.
- Mass of Other Components Specific to Main Landing Gear: This category includes any additional components or structures unique to the main landing gear.