Microjet UAV Ltd
Turbine Technology
FXR150 Turbo-Jet Engine:
| FXR150 Specification | |
|---|---|
| Thrust: | 150 lbs static |
| Maximum rpm: | 79,000 |
| Pressure ratio: | 3.8:1 |
| Fuel Consumption: | 2,500 ml/minute at 150 lbs |
| Fuel Type: | Paraffin or Diesel and 2 stroke oil 2% |
| Dimensions: | 205 mm diameter x 445 mm length |
| Weight: | 19 lbs |
| The FXR150 has a power output of 150 lbs static thrust. This engine is capable of vertical start launch and is supplied with direct kerosene starting. This super high output microturbine has a range of applications including high payload UAV's and static terrestrial power generation. The multi fuel capability and low mass of these engines make them ideal for remote power generation applications. It is also available for the model enthusiast. | |
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For more information on Microjet products, please email
Sarah Ford.
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| Turbo-Shaft | |
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