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  2. Miles per gallon gasoline equivalent - Wikipedia

    en.wikipedia.org/wiki/Miles_per_gallon_gasoline...

    The energy content of gasoline is reduced from 33,705 Wh/gal to 83% of that, or about 27,975 Wh/gal well-to-tank, to account for the energy used in refinement and distribution. Similarly, the energy value for electricity produced from fossil fuel is reduced to 30.3% due to energy lost in generation and transmission, according to the national ...

  3. Gasoline - Wikipedia

    en.wikipedia.org/wiki/Gasoline

    On average, U.S. petroleum refineries produce about 19 to 20 gallons of gasoline, 11 to 13 gallons of distillate fuel diesel fuel and 3 to 4 gallons of jet fuel from each 42 gallon (152 liters) barrel of crude oil. The product ratio depends upon the processing in an oil refinery and the crude oil assay. [17]

  4. List of Volkswagen Group petrol engines - Wikipedia

    en.wikipedia.org/wiki/List_of_Volkswagen_Group...

    two separate water cooling circuits: one of 40 L (8.8 imp gal; 10.6 US gal) capacity utilising three front-mounted radiators, the second of 15 L (3.3 imp gal; 4.0 US gal) for cooling the charged induction air in the two intercoolers aspiration

  5. LMS Ivatt Class 2 2-6-2T - Wikipedia

    en.wikipedia.org/wiki/LMS_Ivatt_Class_2_2-6-2T

    The LMS had various elderly tank engines and the operating department required a new small class 2 locomotive to replace them. Noting that the Great Western Railway 4500 and 4575 Classes of 2-6-2T ('Prairie') had been successful, George Ivatt designed the new engine type incorporating self-emptying ashpans and rocking grates which were labour-saving devices.

  6. Hongdu JL-8 - Wikipedia

    en.wikipedia.org/wiki/Hongdu_JL-8

    The aircraft's fuel system consists of the fuel tanks and the fuel supply/transfer, vent/pressurization, fuel quantity measuring/indicating, fuel refueling and fuel drain subsystems. The total fuel is contained in two fuselage bladder-type rubber tanks and a wing integral tank of 1720 lb. The capacity of each drop tank is 250 litres.

  7. Canadair CL-415 - Wikipedia

    en.wikipedia.org/wiki/Canadair_CL-415

    The aircraft requires 1,340 m (4,400 ft) of flyable length to descend from 15 m (49 ft) altitude, scoop 6,137 L (1,350 imp gal; 1,621 US gal) of water during a twelve-second 410-metre-long (1,350 ft) run on the water at 70 knots (130 km/h; 81 mph), then climb back to 15 m

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