SW800Pro 80‑kg‑Thrust Miniature Turbojet Engine for Civil‑Use UAV

Core Product Advantages

SW800Pro is a high‑performance civilian‑grade miniature turbojet power unit, built for large‑size heavy‑load fixed‑wing aircraft, heavy‑duty civilian unmanned aircraft and high‑speed aerial‑survey equipment. It supplies steady powerful thrust and comes with a full‑set of complete matching electronic‑control parts. Its major advantages are shown below:

Outstanding 80‑kilogram Rated Thrust
This turbojet delivers ample thrust to support large‑scale aircraft take‑off, fast climbing and long‑distance high‑speed cruise. It is well‑suited for heavy‑load aerial‑photography, terrain mapping and long‑range inspection missions.
Optimized Structural Layout
With outer diameter 207.2 mm, overall length 454.7 mm and net‑weight 8400 g, the streamlined housing makes installation simpler and eases the weight burden on the airframe.
Adjustable Wide‑Range Operating Speed
The working rotational‑speed ranges from 25000‑65000 rpm. Operators are allowed to toggle low‑speed cruise and high‑speed flight modes for multiple mission scenarios.
Complete Supporting Accessory Kit
Standard accessories contain ECU, GSU display unit, K7 power plug, K2 signal plug, mounting bracket and fuel pipeline. The whole control system enables parameter setting, real‑time operational‑state monitoring and convenient on‑site debugging.
Convenient Fuel Standard and Low Maintenance Cost
Aviation kerosene acts as the primary fuel mixed with 3%‑5% dedicated lubricating oil. The routine maintenance cycle lasts 25 working hours, effectively cutting the long‑time operating expense of civilian aircraft operators.

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Product Overview

1. Product Positioning for Heavy‑Duty Large‑Scale Civil Fixed‑Wing Aircraft

SW800Pro is a mature miniature turbojet power source designed for civilian unmanned aircraft and large‑size model jets. Compared against piston gasoline engines, the turbojet features fast throttle reaction, excellent high‑altitude adaptability and premium high‑speed flight capability. It is widely applied for long‑range aerial mapping, high‑speed aerial recording and large‑capacity transport unmanned‑air‑vehicles.

2. Physical Index and Flight‑Performance Parameters

Maximum thrust reaches 80 kg, casing outer‑diameter 207.2 mm, full length 454.7 mm and net‑weight 8400 g. Idle speed is 25000 rpm and the top working rotational‑speed hits 65000 rpm. Rated exhaust temperature is 750℃, and the maximum fuel consumption is kept ≤1850 g per minute under standard working‑state.

3. Full‑Set Electronic‑Control Accessories

Every standard package includes ECU controller, GSU monitor, K7 power connector, K2 signal connector, engine fixing bracket and fuel tubing. Users can configure startup settings, acceleration‑deceleration curves, speed limits and temperature thresholds via the control unit.

4. Fine‑Tunable Operating‑Parameter Sheet

Engine Startup Parameters

Oil pump voltage: 0.6‑0.76V
Rotational‑speed slope: 100
Oil pump slope: 2
Hot‑head voltage: 5‑7.6V
Ignition oil‑valve range: 10‑40
Ignition trigger speed: 1300 rpm
Pre‑heating rotational‑speed: 2000 rpm
Clutch separation rotational‑speed: 13000 rpm

Engine Runtime Parameters

Acceleration curve value: 10
Deceleration curve value: 10
Working rotational‑speed scope: 25000‑65000 rpm
Idle rotational‑speed: 25000 rpm
Maximum allowable temperature: ≤1000℃
Working input voltage: ≥10V
Flameout restart function: Disabled
Restart igniter voltage matches the hot‑head working‑voltage
Upper‑limit oil‑pump voltage: 20V

Engine Cooling‑System Parameters

Cooling rotational speed: 2000rpm
Pop‑up response time: 0.8S
Pop‑up working‑voltage: 5V
Continuous‑running voltage: 2.5V

5. Fuel Matching and Daily Maintenance

Aviation kerosene serves as the main fuel, blended with 3%‑5% special lubricant oil. The suggested maintenance cycle is 25 working‑hours. Reasonable fuel proportioning and regular routine inspections can extend the turbojet engine service life.

Technical Parameter Item	Verified Standard Parameter Value
Product Model	SW800Pro
Rated Maximum Thrust	80 kg
Outer Diameter	207.2 mm
Overall Length	454.7 mm
Engine Net Weight	8400 g
Operating Rotational‑Speed Range	25000 ~ 65000 rpm
Idle Rotational‑Speed	25000 rpm
Rated Exhaust Temperature	750℃
Maximum Fuel Consumption	≤1850 g/min
Applicable Fuel	Aviation kerosene
Lubricating‑Oil Mix‑Ratio	3% ~ 5%
Standard Maintenance Cycle	25 working hours
Matched Standard Accessories	ECU, GSU, K7 power plug, K2 signal plug, fixing bracket, oil pipe
Engine Type	Civilian Miniature Turbojet Power‑Plant
Suitable Civil‑Use Scenarios	Heavy‑lift large‑size fixed‑wing aircraft, long‑range aerial‑survey UAV, large‑load civilian unmanned aircraft, high‑speed model jet

Packing & Shipping

Multi‑Layer Shock‑Absorbing Packaging
The turbojet main‑unit, ECU, GSU monitor, connectors and fuel‑system fittings are separately wrapped with shock‑resistant foam. All accessories are placed in a rugged hard‑shell case for protection against vibration damage, dampness and dust during international transportation. Metal components are covered by anti‑scratch protective films.
Full‑Set Standard‑Delivered Attachments
Each shipment comes with the full control‑system kits, installation fasteners, operation manual and fuel‑mixing guide. Spare plugs, pipelines and other replacement accessories are available for custom orders.
Global Multimodal Transportation and Customs‑Ready Documents
We supply ocean shipping, air‑express and door‑to‑door land‑delivery services for overseas aircraft‑model hobbyists, civilian‑UAV manufacturers and aerial‑survey teams. Every parcel contains commercial invoice, packing checklist and factory performance‑test certification to speed‑up overseas customs‑clearance.

Frequently Asked Questions (FAQ)

Q1: What aircraft platforms are compatible with the SW800Pro miniature turbojet engine?

A1: This 80‑kg‑thrust turbojet power‑unit works well for heavy‑load large‑size fixed‑wing model aircraft, long‑distance mapping unmanned‑air‑vehicles and high‑speed civilian aerial‑inspection drones. Its large thrust fits heavy‑duty long‑range flight assignments.

Q2: How to choose fuel and finish parameter debugging?

A2: Adopt aviation kerosene blended with 3%‑5% dedicated lubricant oil. Startup speed, acceleration curves and temperature‑limit settings can be adjusted on the matched ECU‑GSU system. Check the official operation manual for detailed debugging instructions.