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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]
Data from Flying General characteristics Capacity: 2 Length: 22.75 ft (6.93 m) Wingspan: 34.25 ft (10.44 m) Height: 9.25 ft (2.82 m) Wing area: 171.9 sq ft (15.97 m 2) Aspect ratio: 5.2-1 Airfoil: USA35(B) Empty weight: 896 lb (399 kg) Gross weight: 1,320 lb (599 kg) Fuel capacity: 24 US gallons (91 L) usable in 25 US gal (95 L) tank Powerplant: 1 × CC340 horizontally-opposed piston engine ...
The M970 Semi-Trailer Refueler is a 5,000-U.S.-gallon (19,000 L; 4,200 imp gal) fuel dispensing tanker designed for under/overwing refueling of aircraft. It is equipped with a filter/separator, recirculation system and two refueling systems, one for underwing and one for overwing servicing.
Data from Cliche and Virtual Ultralight Museum General characteristics Crew: one Length: 15 ft 0 in (4.57 m) Upper wingspan: 24 ft 0 in (7.32 m) Lower wingspan: 20 ft 4 in (6.20 m) Height: 6 ft 0 in (1.83 m) Wing area: 160 sq ft (15 m 2) Empty weight: 218 lb (99 kg) Gross weight: 415 lb (188 kg) Fuel capacity: 5 U.S. gallons (19 L; 4.2 imp gal) Powerplant: 1 × Cuyuna 430R, 30 hp (22 kW ...
A Panamax container ship can consume 63,000 gallons of marine fuel per day at that speed. Fuel use drops sharply as speeds decrease. A container ship can decrease fuel use close to one-third if it ...
In combustion physics, fuel mass fraction is the ratio of fuel mass flow to the total mass flow of a fuel mixture. If an air flow is fuel free, the fuel mass fraction is zero; in pure fuel without trapped gases, the ratio is unity. [1] As fuel is burned in a combustion process, the fuel mass fraction is reduced. The definition reads as
Data from Cliche and the Virtual Ultralight Museum General characteristics Crew: one Length: 18 ft 4 in (5.59 m) Wingspan: 30 ft 0 in (9.14 m) Height: 7 ft 8 in (2.34 m) Wing area: 152 sq ft (14.1 m 2) Empty weight: 253 lb (115 kg) Gross weight: 550 lb (249 kg) Fuel capacity: 5 U.S. gallons (19 L; 4.2 imp gal) Powerplant: 1 × Kawasaki 440 twin cylinder, two-stroke snowmobile engine, with a ...
Molecular weights of the species in the representative octane combustion are 114, 32, 44, and 18 for C 8 H 18, O 2, CO 2, and H 2 O, respectively; therefore one kilogram (2.2 lb) of fuel reacts with 3.51 kilograms (7.7 lb) of oxygen to produce 3.09 kilograms (6.8 lb) of carbon dioxide and 1.42 kilograms (3.1 lb) of water.