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The Continental IO-360 is a family of fuel-injected air-cooled, horizontally opposed six-cylinder aircraft engines manufactured by Continental Motors in the United States of America, now part of AVIC International since 2010.
The Van's Aircraft RV-8 homebuilt aircraft is often fitted with a 200 hp IO-360 engine. The largest engine that is normally fitted to the Thorp T-18 homebuilt aircraft is the 200 hp IO-360 engine. IO-360-A1A 200 hp (149 kW) at 2700 rpm, Minimum fuel grade 100 or 100LL avgas, compression ratio 8.70:1.
180C with a 210-horsepower (157 kW) Continental IO-360-D engine in a revised cowling, 206 built. M-5-210TC Lunar Rocket 210C fitted with a turbocharged 210-horsepower (157 kW) Lycoming TO-360 engine, 10 built. M-5-220C Lunar Rocket 210C fitted with a 220-horsepower (164 kW) Franklin 6A-350-C1 engine, 57 built. M-5-235C Lunar Rocket
The Lycoming O-360 is a family of four-cylinder, direct-drive, horizontally opposed, air-cooled, piston aircraft engines.Engines in the O-360 series produce between 145 and 225 hp (110 and 170 kW), with the basic O-360 producing 180 hp (130 kW).
[citation needed] Other variants were introduced including the Rocket which is powered by a 210 hp (157 kW) Continental IO-360-A engine, a deluxe Franklin-powered M-4 Astro-Rocket and a Franklin-powered Rocket which is known as the M-4 Strata-Rocket. A STOL variant of the Strata Rocket was developed as the Maule M-5 Lunar Rocket.
Pages in category "Continental aircraft engines" The following 24 pages are in this category, out of 24 total. ... Continental IO-360; Continental IO-370; Continental ...
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In 1929, the company introduced its first aircraft engine, [3] a seven-cylinder radial designated as the A-70, with a displacement of 543.91 cu in (8.91L) that produced 170 hp (127 kW). In August 1929, the Continental Motors Company formed the Continental Aircraft Engine Company as a subsidiary to develop and produce its aircraft engines. [4]
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