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The R-15-300 was designed at the OKB-300 design bureau led by Sergei Tumansky in the late 1950s. The engine was originally intended for the Tupolev Tu-121 high-altitude high-speed cruise missile. Due to a lack of Soviet resources and funding, the engine casing was mainly steel, and in areas exposed to high temperatures, 30-micrometre silver ...
This engine was the first Soviet twin-spool turbojet. It was first run in early 1956 [1] ... R-11V-300 - first production version, high-altitude, non-afterburning;
The Tumansky R-29 is a Soviet turbojet aircraft engine that was developed in the early 1970s. [1] It is generally described as being in the "third generation" of Soviet gas turbine engines which are characterized by high thrust-to-weight ratios and the use of turbine air cooling.
The Tumansky R-13 is a development of the successful Tumansky R-11 engine. It is a two-spool axial-flow turbojet featuring a new five-stage high-pressure compressor, new combustion chamber design to facilitate restarting the engine at high altitudes, new afterburner, and greater use of titanium components.
Engine Components International, Inc. (ECI) is a private aviation piston engine manufacturer. [ citation needed ] It was founded in 1943 as Pennington Channelcromium Co. to support the Army Air Force and Navy during World War II .
The Continental CD-230 is a four-cylinder, horizontally opposed aircraft Diesel engine produced by Continental Motors, Inc. The engine received its type certificate from the US Federal Aviation Administration on December 19, 2012, under the official TD-300-B designation. [1] A later revision adds the TD-300-C with a higher critical altitude. [2]
The PW 300 series has been developed in partnership with MTU who are responsible for the low pressure turbine. The first variant, the PW305A, has the following configuration and was designed with a core flexible enough for engines with take-off thrusts from 20 kN to 31 kN (4,500 to 7,000 lb): a single-stage fan driven by a three-stage low pressure turbine, supercharging a four-stage axial ...
RT300 Jet-A1 Model that runs on Jet A-1 fuel, with a compression ratio of 8.5:1 and produces 31 hp (23 kW) at 7500 rpm. [2]RT300 LCR Model that runs on petroleum or avgas, with a compression ratio of 9.6:1 and produces 32 hp (24 kW) at 7500 rpm.
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