Maximum Fuel Weight in aircraft design represents the maximum weight of fuel that an aircraft can carry for a specific flight while still meeting safety and performance standards. It’s a crucial parameter for flight planning and determining an aircraft’s range. The formula for calculating Maximum Fuel Weight and its SI unit are as follows:
Maximum Fuel Weight Formula: Maximum Fuel Weight can be calculated using the following formula:
- Maximum Fuel Weight: The maximum weight of fuel that the aircraft can carry for a specific flight, measured in kilograms (kg) or pounds (lbs), depending on regional conventions.
- MTOW: Maximum Takeoff Weight, measured in kilograms (kg) or pounds (lbs), representing the maximum weight at which an aircraft is allowed to take off.
- EOW: Empty Operating Weight, which is the weight of the aircraft when it is empty, including the airframe, engines, avionics, and other equipment, measured in kilograms (kg) or pounds (lbs).
- Maximum Payload Weight: The maximum weight of passengers, cargo, and other items that the aircraft can carry, measured in kilograms (kg) or pounds (lbs).