Brandner E-300
The Brandner E-300 was an Egyptian turbojet engine, developed for the Helwan HA-300 light jet fighter.
E-300 | |
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Egyptian E-300 engine undergoing testing | |
Type | Turbojet |
National origin | Egypt |
Manufacturer | Egyptian General Aero Organisation |
Major applications | Helwan HA-300 |
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 attempts to fly it were unsuccessful. The programme of HA-300 was abandoned in May 1969.[2]
Variants
Specifications (variant)
Data from Jane's All The World's Aircraft 1969-70[1]
General characteristics
- Type: Afterburning turbojet
- Length: 4,300 mm (169.3 in)
- Diameter: 840 mm (33 in)
- Dry weight: 860 kg (1,896 lb)
Components
- Compressor: nine-stage axial compressor
- Combustors: can-annular combustion chamber
- Turbine: two-stage axial turbine
Performance
- Maximum thrust: 32.4kN (6,275 lbf) dry, 47.2 kN (10,582 lbf) with reheat
- Overall pressure ratio: 6:1
- Thrust-to-weight ratio: 3.310 dry, 5.581 with reheat
References
- Taylor 1969, p. 671.
- 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
- Taylor, John W. R. Jane's All The World's Aircraft 1969-70. London:Jane's Yearbooks, 1969.