Williams WR24 Turbo-Jet Engine
Small turbojet engine with similar rotating components to the Williams WR9 APU. This relatively common engine could be cosidered to a rival to the British
built Lucas/Rover CT3201 engine.
Williams WR24 Specification
Power Output........................................Up to 200 lbs Thrust depending on the model.
RPM.....................................................52,000
Compressor...........................................Centrifugal Impeller
Combustion Chamber............................Radial Combustion chamber with Rotory Atomiser
Turbine..................................................1 Stage Axial Flow
Layout...................................................Single Spool
Starting..................................................Air Impingement or Cartridge
Ignition.................................................. High Energy Exciter
Fuel System............................... .......... Electric Pump, Electronic Control.
Lubrication............................................Return System, Motor Driven Pump
Oil Spec................................................Aeroshell 390, MIL-L-7808
Accessories...........................................Generator Mounted in Nose
Weight..................................................50 lbs
Application........................................... Drones RPVs,

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