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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.
The F-1 is a rocket engine developed by Rocketdyne.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.
The Saturn AL-31 (originally Lyulka) is a family of axial flow turbofan engines, developed by the Lyulka-Saturn design bureau in the Soviet Union, now NPO Saturn in Russia, originally as a 12.5-tonne (122.6 kN, 27,560 lbf) powerplant for the Sukhoi Su-27 long range air superiority fighter.
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.
The J-2, commonly known as Rocketdyne J-2, was a liquid-fuel cryogenic rocket engine used on NASA's Saturn IB and Saturn V launch vehicles. Built in the United States by Rocketdyne, the J-2 burned cryogenic liquid hydrogen (LH 2) and liquid oxygen (LOX) propellants, with each engine producing 1,033.1 kN (232,250 lb f) of thrust in vacuum.
Diagram of the S-IV second stage of the Saturn I The S-IV second stage was powered by six RL10 rocket engines burning liquid hydrogen (LH 2 ) as fuel with LOX as oxidizer, mounted on gimbals. The propellant tanks used a single, common bulkhead to separate the LOX and LH 2 propellant tanks, saving 20% of structural weight along with the ...
The 2.2-liter Ecotec engine in the 2007 Saturn Ion was improved over the previous year's model: power output increased from 140 hp (104 kW) to 145 hp (108 kW) at 5600 rpm, and torque output increased from 145 lb⋅ft (197 N⋅m) to 150 lb⋅ft (203 N⋅m) at 4200 rpm. The new engine was fitted with the ECU from the 2.4-liter engine.
Eight H-1 engines in a Saturn I. Like all of Rocketdyne's early engines, the H-1 used a waterfall injector fed by turbopumps and regeneratively cooled the engine using the engine's fuel. The combustion chamber was made of 292 stainless steel tubes brazed in a furnace. [12] Unlike the J-2 engine used on the S-IVB stage, the H-1 was a single ...
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