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For this reason, the useful load fraction calculates a similar number, but it is based on the combined weight of the payload and fuel together in relation to the total weight. Propeller-driven airliners had useful load fractions on the order of 25–35%. Modern jet airliners have considerably higher useful load fractions, on the order of 45–55%.
The fraction of payload to the total liftoff weight of the air or spacecraft is known as the "payload fraction". When the weight of the payload and fuel are considered together, it is known as the "useful load fraction". In spacecraft, "mass fraction" is normally used, which is the ratio of payload to everything else, including the rocket ...
The maximum zero fuel weight (MZFW) is the maximum weight allowed before usable fuel and other specified usable agents (engine injection fluid, and other consumable propulsion agents) are loaded in defined sections of the aircraft as limited by strength and airworthiness requirements.
With a fuel fraction of nearly 85%, the GlobalFlyer could carry 5 times its weight in fuel.. In aerospace engineering, an aircraft's fuel fraction, fuel weight fraction, [1] or a spacecraft's propellant fraction, is the weight of the fuel or propellant divided by the gross take-off weight of the craft (including propellant): [2]
The weight of the aircraft is the common factor that links all aspects of aircraft design such as aerodynamics, structure, and propulsion, all together. An aircraft's weight is derived from various factors such as empty weight, payload, useful load, etc. The various weights are used to then calculate the center of mass of the entire aircraft. [37]
The aircraft has a typical empty weight of 1,354 lb (614 kg) and a gross weight of 1,954 lb (886 kg), giving a useful load of 600 lb (270 kg). With full fuel of 41 U.S. gallons (160 L; 34 imp gal) the payload for pilot and baggage is 354 lb (161 kg). [1]
Nelson shares her Apple Watch stats: ‘For that 20-minute low-impact indoor walking workout, I burned 186 calories, and my average heart was 145bpm.
The CASA C-212 Aviocar is a turboprop-powered STOL medium cargo aircraft designed and built by the Spanish aircraft manufacturer Construcciones Aeronáuticas SA (CASA). It is designed for use by both civil and military operators.