Rolls-Royce/MAN Turbo RB153
| RB.153 | |
|---|---|
| Type | Turbofan |
| Manufacturer | Rolls-Royce Limited MAN Turbo |
| First run | January 1963 |
| Major applications | EWR VJ 101D |
The Rolls-Royce/MAN Turbo RB.153 was a high-performance 6,850 pounds-force (3,110 kgf) dry thrust turbofan engine developed jointly by Rolls-Royce Limited and MAN Turbo.[1] Developed for the German EWR VJ 101D interceptor with a German-developed thrust-deflector system.[1] The engine was also proposed for a number of other military VTOL projects including the Hawker P.1157. A commercial-version of the engine was also considered for the Messerschmitt Me P.160 airliner.[1] The VJ101D project was cancelled and the engine never flew, being retained as a test bed.
Applications
- EWR VJ 101D cancelled.[1]
Specifications
General characteristics
- Type: Turbofan
- Length: 89 inches (2.261 metres)
- Diameter: 29.5 inches (0.749 metres)
- Dry weight: 1431 lb (649 kg)
Components
- Compressor:
Performance
- Maximum thrust: 6,850 lbf (3,110 kgf) (3,0470 N)
- Fuel consumption: 121 lb/s (54.9 kg/s)
- Power-to-weight ratio:
See also
- Related lists
References
- Notes
- 1 2 3 4 "R-R/MAN RB.153". Flight International: 908–909. 5 December 1963.
Turbofan and turbojet engines: database handbook p395 (2007) By Élodie Roux
This article is issued from
Wikipedia.
The text is licensed under Creative Commons - Attribution - Sharealike.
Additional terms may apply for the media files.