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Turbojet Engine special for fixed wing drone with large Thrust-to-Weight Ratio of 8.1

Τόπος καταγωγής:Κίνα
Επωνυμία:Zhongdeng
Αριθμός μοντέλου:ZD-TBE-85
Λεπτομέρειες για το προϊόν
Επισημαίνω:

fixed wing drone turbojet engine

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turbojet engine 8.1 thrust-to-weight ratio

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large thrust drone turbojet engine
Maximum Thrust: 85 κιλά
Thrust-To-Weight Ratio: 8.1
Weight: 10,5 κιλά
Operating Mach Number: 0.9mA
Fuel Consumption At Maximum Thrust: 2,40 L/min
Fuel Type: Κηροζίνη αεροπορίας (3~5% λιπαντικό αναμεμειγμένο)
Περιγραφή του προϊόντος
Turbojet Engine for Fixed-Wing Drones — 85 kgf Class The 85 kgf turbojet engine is engineered as a compact power unit for small fixed-wing aircraft and unmanned aerial vehicles. Under International Standard Atmosphere conditions at sea level with Mach 0, it delivers a maximum static thrust of approximately 90 kgf, achieving a thrust-to-weight ratio of 8.1. The engine assembly comprises an air inlet, axial compressor, annular combustion chamber, turbine stage, and converging
Σύνοψη του προϊόντος

Turbojet Engine for Fixed-Wing Drones — 85 kgf Class The 85 kgf turbojet engine is engineered as a compact power unit for small fixed-wing aircraft and unmanned aerial vehicles. Under International Standard Atmosphere conditions at sea level with Mach 0, it delivers a maximum static thrust of ...

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