Quote: Originally posted by telford_mike on 31 January 2003
This ought to do it:
http://www.gasturbine.pwp.blueyonder.co.uk/derwent1.jpg
Power Output....................................3500 Lbs Static Thrust
RPM.................................................14,700 rpm
Compressor.......................................Dual Sided Centrifugal Impeller with Radial Inducer Vanes
Combustion Chamber........................9 thru-flow can type combustion chambers, Duplex Burners
Compressor Turbine..........................1 Stage Axial
Layout...............................................Single Spool Turbo-Jet with accessory gearbox at front.
Starting..............................................Rotax Electric Starter
Ignition..............................................High Tension Torch Ignitors
Fuel System...................................... Piston Pump with Hydromechanical Governor, Barometric (Altitude) Control Unit
Oil System.........................................Return System with Pressure and Scavenge pumps, Intergral Oil Tank.
Accessories.......................................Cooling Fan Mounted on centre shaft, External Airframe Mounted A/Gearbox
Weight..............................................1300 Lbs
Applications......................................Gloster Meteor Aircraft, Renault Clio