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This one-cylinder engine was designated "Hyper No. 2", and became the test bed for developing the cylinders that would become the Continental O-1430 ("O" for "opposed") engine. It would require a ten-year development period which changed the layout to first an upright V-12 engine and later, an inverted V-12 engine, before becoming reliable ...
The 130 hp (97 kW) O-240 was a new engine design derived from the six-cylinder Continental O-360 and introduced in 1971. It is generally similar in overall dimensions to the Continental O-200, but with a higher 8.5:1 compression ratio, designed to run on 100/130 avgas.
The Continental IO-370 engine is a family of fuel injected four-cylinder, horizontally opposed, air-cooled aircraft engines that were developed for use in light aircraft by Continental Aerospace Technologies. There is no carbureted version of this engine, which would have been designation O-370, therefore the base model is the IO-370. [1]
This page is an incomplete list of orbital rocket engine data and specifications. Current, upcoming, and in-development rocket engines ... IV, SLS: Active Upper LH 2 ...
The Lycoming IO-580 engine is a horizontally opposed, six-cylinder aircraft engine featuring three cylinders per side, manufactured by Lycoming Engines. [1] There is no carburetted version of the engine, which would have been designated O-580 and therefore the base model is the IO-580. [2] This engine family competes with the Continental IO-550 ...
An E-8 crew member entering data using an AN/PYQ-10 before a flight The AN/PYQ-10 Simple Key Loader (SKL) is a ruggedized, portable, hand-held fill device , for securely receiving, storing, and transferring data between compatible cryptographic and communications equipment.
The IO-390 was developed from the similar IO-360 engine, by using cylinders from the IO-580 [citation needed] to increase the O-360's cylinder bore. (Although the IO-390 cylinder assembly [4] is not the same part number as the IO-580, [5] the cylinder barrels of both have a 5.318 bore and 4.375 stroke dimension.)
The engine has a displacement of 541.5 cubic inches (8.87 litres) and produces a maximum of 450 hp (336 kW) in its TIGO-541 version. The cylinders have air-cooled heads. [1] [2] The first TIO-541-A1A was type certified on 23 February 1965 on the regulatory basis of CAR 13 effective 15 June 1956 as amended to 13-1 through 13-4. [1]