Microjet UAV Ltd
Turbine Technology
FXR00 Turbo-Jet Engine:
| FXR100 Specification | |
|---|---|
| Thrust: | 95 lbs static |
| Maximum rpm: | 89,000 |
| Pressure ratio: | 4:1 |
| Fuel Consumption: | 1,400 ml/minute at 95 lbs |
| Fuel Type: | Paraffin or Diesel and 2 stroke oil 2% |
| Dimensions: | 154 mm diameter x 383 mm length |
| Weight: | 10.4 lbs |
| To meet the demands of increased performance and payloads for modern UAV's, the FXR100 was developed. The design is based on the casing diameters of the HF65 unit, this - combined with significantly improved power output to 95 lbs - has resulted in an extremely superior engine which has been employed in a number of reconnaissance vehicle and high speed drone applications, as well as the traditional model aeroplane markets which we've been active in for so long. To date the FXR100 is our most popular engine. | |
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For more information on Microjet products, please email
Sarah Ford.
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The HF100 Engine with re-heat
| FXR150 | |
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