Brandner E-300

Last updated
E-300
Brandner E-300 engine.jpg
Egyptian E-300 engine undergoing testing
Type Turbojet
National origin Egypt
ManufacturerEgyptian General Aero Organisation
Major applications Helwan HA-300

The Brandner E-300 was an Egyptian turbojet engine, developed for the Helwan HA-300 light jet fighter.

Contents

Development

Austrian engineer Ferdinand Brandner, who had worked in the Soviet Union, leading the development of the Kuznetsov NK-12 turboprop, the powerplant of the Tupolev Tu-95 bomber, moved to Egypt to lead a team to design an engine to power the Helwan HA-300 jet fighter that was simultaneously being designed by a team of Germans led by Willy Messerschmitt.

The new engine underwent bench testing in 1963, and was flight tested under the wing of an Antonov An-12, before being installed in a HAL HF-24 Marut for high speed testing, in which form it flew on 29 March 1967. [1] The E-300 was installed in the third HA-300 prototype (the first two were powered by Bristol Siddeley Orpheus engines), but testing stopped in the taxi-test stage before flight tests. The programme of HA-300 was abandoned in May 1969. [2]

Variants

E-300-A
Military version for HA-300
E-300-C1
Civil version of E-300-A, proposed for Project 206 three-engined airliner. [1]
E-300-C2
Proposed growth version of E-300-C1. [1]
E-300-AF
Projected turbofan development. [1]

Specifications (variant)

Data from Jane's All The World's Aircraft 1969-70 [1]

General characteristics

Components

Performance

Related Research Articles

<span class="mw-page-title-main">Turbojet</span> Airbreathing jet engine which is typically used in aircraft

The turbojet is an airbreathing jet engine which is typically used in aircraft. It consists of a gas turbine with a propelling nozzle. The gas turbine has an air inlet which includes inlet guide vanes, a compressor, a combustion chamber, and a turbine. The compressed air from the compressor is heated by burning fuel in the combustion chamber and then allowed to expand through the turbine. The turbine exhaust is then expanded in the propelling nozzle where it is accelerated to high speed to provide thrust. Two engineers, Frank Whittle in the United Kingdom and Hans von Ohain in Germany, developed the concept independently into practical engines during the late 1930s.

<span class="mw-page-title-main">Junkers Jumo 004</span> Early turbojet aircraft engine

The Junkers Jumo 004 was the world's first production turbojet engine in operational use, and the first successful axial compressor turbojet engine. Some 8,000 units were manufactured by Junkers in Germany late in World War II, powering the Messerschmitt Me 262 fighter and the Arado Ar 234 reconnaissance/bomber, along with prototypes, including the Horten Ho 229. Variants and copies of the engine were produced in Eastern Europe and the USSR for several years following the end of WWII.

<span class="mw-page-title-main">BMW 003</span> Early German axial turbojet engine

The BMW 003 is an early axial turbojet engine produced by BMW AG in Germany during World War II. The 003 and the Junkers Jumo 004 were the only German turbojet engines to reach production during World War II.

<span class="mw-page-title-main">General Electric J79</span> Axial flow turbojet engine

The General Electric J79 is an axial-flow turbojet engine built for use in a variety of fighter and bomber aircraft and a supersonic cruise missile. The J79 was produced by General Electric Aircraft Engines in the United States, and under license by several other companies worldwide. Among its major uses was the Lockheed F-104 Starfighter, Convair B-58 Hustler, McDonnell Douglas F-4 Phantom II, North American A-5 Vigilante and IAI Kfir.

<span class="mw-page-title-main">Allison J35</span>

The General Electric/Allison J35 was the United States Air Force's first axial-flow compressor jet engine. Originally developed by General Electric in parallel with the Whittle-based centrifugal-flow J33, the J35 was a fairly simple turbojet, consisting of an eleven-stage axial-flow compressor and a single-stage turbine. With the afterburner, which most models carried, it produced a thrust of 7,400 lbf (33 kN).

<span class="mw-page-title-main">Rolls-Royce Avon</span> 1940s British turbojet aircraft engine

The Rolls-Royce Avon was the first axial flow jet engine designed and produced by Rolls-Royce. Introduced in 1950, the engine went on to become one of their most successful post-World War II engine designs. It was used in a wide variety of aircraft, both military and civilian, as well as versions for stationary and maritime power.

<span class="mw-page-title-main">Metropolitan-Vickers F.2</span> Early turbojet engine

The Metropolitan-Vickers F.2 is an early turbojet engine and the first British design to be based on an axial-flow compressor. It was an extremely advanced design for the era, using a nine-stage axial compressor, annular combustor, and a two-stage turbine.

<span class="mw-page-title-main">Armstrong Siddeley Sapphire</span> 1940s British turbojet aircraft engine

The Armstrong Siddeley Sapphire is a British turbojet engine that was produced by Armstrong Siddeley in the 1950s. It was the ultimate development of work that had started as the Metrovick F.2 in 1940, evolving into an advanced axial flow design with an annular combustion chamber that developed over 11,000 lbf (49 kN). It powered early versions of the Hawker Hunter and Handley Page Victor, and every Gloster Javelin. Production was also started under licence in the United States by Wright Aeronautical as the J65, powering a number of US designs. The Sapphire's primary competitor was the Rolls-Royce Avon.

<span class="mw-page-title-main">Heinkel HeS 011</span> German turbojet engine

The Heinkel HeS 011 or Heinkel-Hirth 109-011(HeS - Heinkel Strahltriebwerke) was an advanced World War II jet engine built by Heinkel-Hirth. It featured a unique compressor arrangement, starting with a low-compression impeller in the intake, followed by a "diagonal" stage similar to a centrifugal compressor, and then a three-stage axial compressor. Many of the German jet-powered aircraft being designed near the end of the war were designed to use the HeS 011, but the engine itself was not ready for production before the war ended in Europe and only small numbers of prototypes were produced.

<span class="mw-page-title-main">Snecma M53</span>

The SNECMA M53 is an afterburning turbofan engine developed for the Dassault Mirage 2000 fighter by Snecma. The engine is in service with different air forces, including the latest Mirage 2000-5 and 2000-9 multirole fighters.

<span class="mw-page-title-main">Lyulka AL-7</span>

The Lyulka AL-7 was a turbojet designed by Arkhip Mikhailovich Lyulka and produced by his Lyulka design bureau. The engine was produced between 1954 and 1970.

<span class="mw-page-title-main">General Electric CJ610</span> Turbojet engine

The General Electric CJ610 is a non-afterburning turbojet engine derived from the military J85, and is used on a number of civilian business jets. The model has logged over 16.5 million hours of operation. Civilian versions have powered business jets such as the Learjet 23 and the Hamburger Flugzeugbau HFB 320 Hansa Jet. The engines are also used in the flyable Messerschmitt Me 262 reproductions built by the Me 262 Project in the United States.

<span class="mw-page-title-main">Bristol Siddeley Orpheus</span> 1957 turbojet aircraft engine family by Bristol Siddeley

The Bristol Siddeley Orpheus is a single-spool turbojet developed by Bristol Siddeley for various light fighter/trainer applications such as the Folland Gnat and the Fiat G.91. Later, the Orpheus formed the core of the first Bristol Pegasus vectored thrust turbofan used in the Harrier family.

<span class="mw-page-title-main">Helwan HA-300</span> Egyptian interceptor aircraft prototype

The Helwan HA-300 was a single-engine, delta-wing, light supersonic interceptor aircraft developed in Egypt during the 1960s.

The Avro Canada TR.4 Chinook was Canada's first turbojet engine, designed by Turbo Research and manufactured by A.V. Roe Canada Ltd. Named for the warm Chinook wind that blows in the Rocky Mountains, only three Chinooks were built and none were used operationally. After being scaled up from 2,600 lbf (12 kN) to 6,500 lbf (29 kN), it would become the Orenda.

<span class="mw-page-title-main">Rolls-Royce/Snecma Olympus 593</span> 1960s British/French turbojet aircraft engine

The Rolls-Royce/Snecma Olympus 593 was an Anglo-French turbojet with reheat, which powered the supersonic airliner Concorde. It was initially a joint project between Bristol Siddeley Engines Limited (BSEL) and Snecma, derived from the Bristol Siddeley Olympus 22R engine. Rolls-Royce Limited acquired BSEL in 1966 during development of the engine, making BSEL the Bristol Engine Division of Rolls-Royce.

<span class="mw-page-title-main">Power Jets W.2</span> British turbojet engine

The Power Jets W.2 was a British turbojet engine designed by Frank Whittle and Power Jets Ltd. Like the earlier Power Jets W.1, the reverse-flow combustion configuration included a double-sided centrifugal compressor, 10 combustion chambers and an axial-flow turbine with air-cooled disc. It entered production as the Rolls-Royce Welland and was the first UK jet engine to power operational aircraft, the Gloster Meteor.

<span class="mw-page-title-main">Rolls-Royce RB.145</span> 1960s British turbojet aircraft engine

The Rolls-Royce RB.145 was a British jet engine designed in the early-1960s by Rolls-Royce for use as a lightweight VTOL lift and cruise engine. Developed from the Rolls-Royce RB108 the RB.145 featured more accessories and a higher thrust rating. Six engines developed by MAN Turbo were fitted to the first prototype of the EWR VJ 101 experimental German fighter aircraft, achieving supersonic flight by July 1964.

The Packard XJ49 was the first U.S. designed turbofan aircraft engine, and was developed by the Packard Motor Co. in the 1940s.

<span class="mw-page-title-main">STAL Dovern</span> 1950s Swedish turbojet aircraft engine

The STAL Dovern was a Swedish turbojet design of the early 1950s, named after a lake in Finspång municipality in Östergötland, Sweden. Intended to power the Saab 35 Draken, this aircraft was powered by the Rolls-Royce Avon instead. The Dovern did not enter production.

References

  1. 1 2 3 4 5 Taylor 1969, p. 671.
  2. Group Captain Kapil Bhargava. "Messerschmitt's HA-300 and its Indian Connection". Memoirs. Indian Air Force. Archived from the original on 2008-07-05. Retrieved 2008-08-08.

Bibliography