Brandner E-300
| E-300 | |
|---|---|
 | |
| Egyptian E-300 engine underwent testing | |
| Type | Turbojet |
| National origin | Egypt |
| Manufacturer | Egyptian 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.
Development
Austrian engineer Ferdinand Brandner, who had worked as a Soviet prisoner on 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), it flew at least one time and successfully, but 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
- 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
- Power-to-weight ratio: 3.310 dry, 5.581 with reheat
References
Bibliography
- Taylor, John W. R. Jane's All The World's Aircraft 1969-70. London:Jane's Yearbooks, 1969.