This is a list of all German motors including all aircraft engines, rocket motors, jets and any other powerplants, along with a very basic description. It includes experimental engines as well as those that made it to production status.
The Reich Air Ministry used an internal designation system that included a prefix number signifying the engine type, 9 for piston engines and 109 for jets and rockets, followed by a manufacturer's code, followed by an engine series number.[1] Unlike the 9-prefixed piston engine designations, the 109-series of reaction-thrust, turbojet, turboprop and rocket engine designation numbers' three-place numerical suffixes had no "firm adherence" to any one manufacturer.
Using this system, the famous BMW engine used in the Focke-Wulf Fw 190 would be known as the 9-801 (Piston(9)-BMW(8)Number(01)). However, this system was not widely used, even within the RLM, and a common name consisting of the manufacturer's name (often abbreviated) followed by the model number was much more common. The list below uses the common BMW 801 instead of the official 9-801.
Engines produced before the RLM's designation system was set up are often listed using the same basic terminology. So while the interwar Argus 10 engine can be referred to as the As 10, it is not correct to call it the 9–10, this designation was never applied.
The Luftwaffe also used engines from France, particularly the Gnôme-Rhône 14 cylinder series of radial engines for its Henschel Hs 129 (14M) ground attack aircraft and Messerschmitt Me 323 (14N) "Gigant" transporter.
Daimler-Benz DB 602 16-cylinder diesel powered the two Hindenburg class airships
Daimler-Benz DB 603 "enlarged DB601" (largest displacement German inverted V12) for use in bombers and fighter-bombers, little fighter use
Daimler-Benz DB 604 prototype 24-cylinder (X-24) engine, cancelled in September 1942
Daimler-Benz DB 605 improved and slightly enlarged DB601 for use in fighters
Daimler-Benz DB 606 First conceived in February 1937; composed of twinned DB 601 engines, a 1.5 tonne weight coupled "power system", derided as a "welded-together engine" by Goering in August 1942
Daimler-Benz DB 613 First conceived in March 1940; two coupled "power system" DB603 engines, total weight of 1.8 tonnes apiece, as with the 606 and 610, experimental only
Jumo 222 key engine program for German military aircraft: experimental 24-cylinder supercharged liquid-cooled "star" (6 banks, of 4 cylinders apiece) aircraft engine; nearly 300 examples built
(Rocket engines, turboprops, turbojets, and other non-piston engines included) For the Last three digits: 001-499 Air Breathing, 500–999 Non-Air Breathing (Rockets)
109-448BMW-built liquid-fuel rocket, intended for the Ruhrstahl X-4 wire-guided air-to-air missile
109-500Walter, self-contained Starthilfe monopropellant RATO unit, jettisonable following take-off with parachute recovery
109-501 Walter, an experimental uprated Starthilfe RATO unit similar to the -500 model, but with 1,500 kgf (3,300 lb) thrust that also used a kerosene/hydrazine-base fuel with the T-Stoff[2]
The BMW 801 was a powerful German 41.8-litre (2,550 cu in) air-cooled 14-cylinder-radial aircraft engine built by BMW and used in a number of German Luftwaffe aircraft of World War II. Production versions of the twin-row engine generated between 1,560 and 2,000 PS. It was the most produced radial engine of Germany in World War II with more than 61,000 built.
Bomber B was a German military aircraft design competition organised just before the start of World War II intended to develop a second-generation high-speed bomber for the Luftwaffe. The new designs would be a direct successor to the Schnellbomber philosophy of the Dornier Do 17 and Junkers Ju 88, relying on high speed as its primary defence. Bomber B would be a much larger and more capable aircraft, with range and payload far greater than the Schnellbomber, surpassing the largest conventional designs then under consideration. The winning design was intended to form the backbone of the Luftwaffe's bomber force, replacing the wide collection of semi-specialized designs then in service. The Reich Air Ministry was so optimistic that more modest projects were generally cancelled; when the project failed the Luftwaffe was left with hopelessly outdated aircraft.
The Jumo 222 was a German high-power multiple-bank in-line piston aircraft engine from Junkers, designed under the management of Ferdinand Brandner of the Junkers Motorenwerke.
The Jumo 211 was a German inverted V-12 aircraft engine, Junkers Motoren's primary aircraft engine of World War II. It was the direct competitor to the Daimler-Benz DB 601 and closely paralleled its development. While the Daimler-Benz engine was mostly used in single-engined and twin-engined fighters, the Jumo engine was primarily used in bombers such as Junkers' own Ju 87 and Ju 88, and Heinkel's H-series examples of the Heinkel He 111 medium bomber. It was the most-produced German aero engine of the war, with almost 70,000 examples completed.
The Me 209 of 1943 was an attempt to create an enhanced version of the Bf 109, which served as the Luftwaffe's primary fighter aircraft throughout World War II. The Me 209, despite its designation, bore no relationship to the earlier Me 209.
The BMW 803 was a German aircraft engine, an attempt by BMW to build a high-output aircraft engine by coupling two BMW 801 engines back-to-back, driving contra-rotating propellers. The result was a 28-cylinder, four-row radial engine, each comprising a multiple-bank in-line engine with two cylinders in each bank, which, due to cooling concerns, were liquid cooled.
The BMW 802 was a large air-cooled radial aircraft engine, built using two rows of nine cylinders to produce what was essentially an 18-cylinder version of the 14-cylinder BMW 801. Although promising at first, development dragged on and the project was eventually cancelled to concentrate on jet engines instead.
The Junkers Jumo 213 was a World War II-era V-12 liquid-cooled aircraft engine, a development of Junkers Motoren's earlier design, the Jumo 211. The design added two features, a pressurized cooling system that required considerably less cooling fluid which allowed the engine to be built smaller and lighter, and a number of improvements that allowed it to run at higher RPM. These changes boosted power by over 500 hp and made the 213 one of the most sought-after Axis engine designs in the late-war era.
The Jumo 210 was Junkers' first production inverted V12 gasoline aircraft engine, first produced in the early 1930s. Depending on the version it produced between 610 and 730 PS and can be considered a counterpart of the Rolls-Royce Kestrel in many ways. Although originally intended to be used in almost all pre-war designs, rapid progress in aircraft design quickly relegated it to the small end of the power scale by the late 1930s. Almost all aircraft designs switched to the much larger Daimler-Benz DB 600, so the 210 was produced only for a short time before Junkers responded with a larger engine of their own, the Junkers Jumo 211.
The Daimler-Benz DB 600 was a German aircraft engine designed and built before World War II as part of a new generation of German engine technology. It was a liquid-cooled inverted V12 engine, and powered the Messerschmitt Bf 110 and Heinkel He 111 among others.
The Daimler-Benz DB 605 is a German aircraft engine built during World War II. Developed from the DB 601, the DB 605 was used from 1942 to 1945 in the Messerschmitt Bf 109 fighter, and the Bf 110 and Me 210C heavy fighters.
The Daimler-Benz DB 603 was a German aircraft engine used during World War II. It was a liquid-cooled 12-cylinder inverted V12 enlargement of the 33.9 Liter DB 601, which was in itself a development of the DB 600. Production of the DB 603 commenced in May 1942, and with a 44.5 liter displacement figure, was the largest displacement inverted V12 aviation engine to be produced and used in front line aircraft of the Third Reich during World War II.
The Henschel Hs 130 was a German high-altitude reconnaissance and bomber aircraft developed in World War II. It suffered from various mechanical faults and was never used operationally, only existing as prototype airframes.
The Armstrong Siddeley Hyena was a British aero engine developed by Armstrong Siddeley. Designed in the 1930s, it was an unusual experimental radial engine with inline cylinder banks. It was flown using an Armstrong Whitworth A.W.16 fighter aircraft as a test bed. Unresolved problems with cooling of the rear cylinders prevented the engine from going into production. Few details of this engine survive as company records were lost.
In aviation, an inline engine is a reciprocating engine with banks of cylinders, one behind another, rather than rows of cylinders, with each bank having any number of cylinders, although more than six is uncommon. The major reciprocating-engine alternative configuration is the radial engine, where the cylinders are placed in a circular or "star" arrangement.
The Daimler-Benz DB 604 was an experimental German 24-cylinder aircraft engine, which did not progress beyond the initial engine testing phase and was ultimately abandoned in 1942.
The Daimler-Benz DB 600 series were a number of German aircraft engines designed and built before and during World War II as part of a new generation of German engine technology. The general layout was that of a liquid-cooled, inverted V12 engine. The design originated to a private venture project of Daimler-Benz, the F4 engine. Most newer DB engine designs used in WW2 were based around this engine.
The Kawasaki Ha40, also known as the Army Type 2 1,100 hp Liquid Cooled In-line and Ha-60, was a license-built Daimler-Benz DB 601Aa 12-cylinder liquid-cooled inverted-vee aircraft engine. The Imperial Japanese Army Air Service (IJAAS) selected the engine to power its Kawasaki Ki-61 fighter.
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