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The differences between Jet A and Jet A-1 are twofold. The primary difference is the lower freezing point of Jet A-1 fuel: [5] Jet A's is −40 °C (−40 °F) Jet A-1's is −47 °C (−53 °F) The other difference is the mandatory addition of an antistatic additive to Jet A-1 fuel.
Since these tanks are part of the aircraft structure, they cannot be removed for service or inspection. Inspection panels must be provided to allow internal inspection, repair, and overall servicing of the tank. Most large transport aircraft use this system to store fuel in the wings, fuselage and empennage of the aircraft. [1]
The Gulfstream G650 is a large business jet produced by Gulfstream Aerospace. [3] The model is designated Gulfstream GVI in its type certificate. [4] The aircraft can be configured to carry from 11 to 18 passengers over a range of 7,000 nautical miles [nmi] (13,000 km; 8,100 mi) at a top speed of Mach 0.925 (530.6 kn; 982.7 km/h; 610.6 mph).
In 2019, 0.1% of fuel was SAF: [36] The International Air Transport Association (IATA) supported the adoption of Sustainable Aviation fuel, aiming in 2019 for 2% share by 2025: 7 million m 3 (1.8 billion US gal). [37] [19] In 2019, United Airlines purchased up to 10 million US gallons (38,000 m 3) of SAF from World Energy over two years. [38]
The Argus As 014 (designated 109-014 by the RLM) was a pulsejet engine used on the German V-1 flying bomb of World War II, and the first model of pulsejet engine placed in mass production. License manufacture of the As 014 was carried out in Japan in the latter stages of World War II, as the Kawanishi Maru Ka10 for the Kawanishi Baika kamikaze jet.
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JP-10 fuel (Jet Propellant 10) is a jet fuel, specified and used mainly as fuel in missiles. Being designed for military purposes, it is not a kerosene based fuel. Developed to be a gas turbine fuel for cruise missiles , [ 1 ] it contains mainly exo-tetrahydrodicyclopentadiene (a synthetic fuel ), and adamantane .
Jet fuel can contain a small amount of dissolved water that does not appear in droplet form. As an aircraft gains altitude, the temperature drops and the fuel's capacity to hold water is diminished. As an aircraft gains altitude, the temperature drops and the fuel's capacity to hold water is diminished.