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  2. Fuel siphoning sucks! Protect yourself with a locking gas cap!

    www.aol.com/2008/05/28/fuel-siphoning-sucks...

    When I was a kid, my buddy Sean had a huge collection of 1970's-era MAD magazines. I remember flipping through them, laughing at the Star Wars and Jaws jokes, and being totally puzzled by the gas ...

  3. Vapor lock - Wikipedia

    en.wikipedia.org/wiki/Vapor_lock

    Vapor lock is a problem caused by liquid fuel changing state to vapor while still in the fuel delivery system of gasoline-fueled internal combustion engines.This disrupts the operation of the fuel pump, causing loss of feed pressure to the carburetor or fuel injection system, resulting in transient loss of power or complete stalling.

  4. Rocketdyne F-1 - Wikipedia

    en.wikipedia.org/wiki/Rocketdyne_F-1

    The engine uses a gas-generator cycle developed in the United States in the late 1950s and was used in the Saturn V rocket in the 1960s and early 1970s. Five F-1 engines were used in the S-IC first stage of each Saturn V, which served as the main launch vehicle of the Apollo program .

  5. Mitsubishi Saturn engine - Wikipedia

    en.wikipedia.org/wiki/Mitsubishi_Saturn_engine

    The Mitsubishi Saturn or 4G3 engine is series of overhead camshaft (OHC) straight-four internal combustion engines introduced by Mitsubishi Motors and saw first service in the 1969 Colt Galant. Displacement ranges from 1.2 to 1.8 L (1,239 to 1,755 cc), although there was also a rare 2-litre (1,994 cc) inline-six version built from 1970 until 1976.

  6. Saturn I4 engine - Wikipedia

    en.wikipedia.org/wiki/Saturn_I4_engine

    The powerplant used in Saturn S-Series automobiles was a straight-4 aluminum piston engine produced by Saturn, a subsidiary of General Motors. The engine was only used in the Saturn S-series line of vehicles (SL, SC, SW) from 1991 through 2002. It was available in chain-driven SOHC or DOHC variants.

  7. Rocketdyne H-1 - Wikipedia

    en.wikipedia.org/wiki/Rocketdyne_H-1

    The Rocketdyne H-1 was a 205,000 lbf (910 kN) thrust liquid-propellant rocket engine burning LOX and RP-1.The H-1 was developed for use in the S-I and S-IB first stages of the Saturn I and Saturn IB rockets, respectively, where it was used in clusters of eight engines.