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JP-4 froze at −76 °F (−60 °C), and its maximum burning temperature was 6,670 °F (3,688 °C). [citation needed] JP-4 was a non-conductive liquid, prone to build up static electricity when being moved through pipes and tanks. As it is volatile and has a low flash point, the static discharge could cause a fire. Beginning in the mid-1980s an ...
JP-8 is a jet fuel, specified and used widely by the U.S. military. It is specified by MIL-DTL-83133 and British Defence Standard 91-87. JP-8 is a kerosene-based fuel, projected to remain in use at least until 2025. The United States military uses JP-8 as a "universal fuel" in both turbine-powered aircraft and diesel-powered ground vehicles.
JP-8, or JP8 (for "Jet Propellant 8"), is a jet fuel, specified and used widely by the US military. It is specified by MIL-DTL-83133 and British Defence Standard 91-87, and similar to commercial aviation's Jet A-1 , but with the addition of corrosion inhibitor and anti-icing additives.
The explosion took place in an underground storage tank containing JP-4, a military jet fuel blend. The toll was 34 dead, 2 injured, 3 missing. [ 1 ] The explosion was caused by the deliberate activation of a novel carbon dioxide fire extinguishment system during an acceptance test as part of final commissioning.
Toxic: a chemical that has a median lethal concentration (LC 50) in air of more than 200 parts per million (ppm) but not more than 2,000 parts per million by volume of gas or vapor, or more than 2 milligrams per liter but not more than 20 milligrams per liter of mist, fume or dust, when administered by continuous inhalation for 1 hour (or less if death occurs within 1 hour) to albino rats ...
The AR2 is a single-chamber rocket engine burning kerosene (JP-4 or JP-5) jet fuel, oxidised with 90% High Test Peroxide (H 2 O 2 / HTP), allowing the engine to use the same fuel as an aircraft fuel system. [1] The variable-thrust AR2 is a direct development of the fixed thrust AR1, which was given the military designation LR36.
A single Sabre 3 was built with the Orenda 4 engine, with performance similar to the US models. Production then turned to the Sabre 5 with the Orenda 10, and then to the Sabre 6 with the Orenda 11-derived 7,500 lbf (33,000 N) thrust Orenda 14. The resulting Sabre was both lighter and more powerful than its J47 powered counterparts, and went on ...
Fuel type: aviation kerosene / JP-4; Oil system: pressure spray with scavenge at 40 psi (280 kPa) Performance. Maximum thrust: dry 7,250 lbf (32.2 kN) thrust for take ...