Product Overview
This 130N micro turbojet UAV engine is a high-performance liquid-fuel drone gasoline engine customized for professional civilian unmanned aerial vehicle platforms. As a compact jet-type UAV gasoline engine, it balances lightweight dimensions and powerful 13kg static thrust, perfectly matching high-speed fixed-wing civilian drones, aerial survey aircraft and large RC aviation models.
Different from conventional piston UAV engines, this turbojet power unit adopts fully automatic fuel ignition without external startup auxiliary equipment. It supports multi-type civilian fuels including aviation kerosene and standard diesel, offering flexible fuel supply options for global commercial operators. Its integrated anti-vibration, anti-corrosion and low-consumption design lowers overall operation costs for civilian aerial mapping, high-speed inspection and educational aviation projects.
All design and manufacturing standards target purely non-military commercial scenarios, providing stable, long-endurance thrust for civilian industrial UAV fleets and private large aviation models.
Complete Technical Specification Table
| Specification Item | Exact Parameter |
|---|---|
| Static Max Thrust | 130 N / 13 kgf |
| Net Engine Weight | 1630 g |
| Outer Diameter | 110 mm |
| Overall Length | 290 mm |
| Maximum Limit RPM | 115000 rpm |
| Stable Idle RPM | 36000 rpm |
| Maximum Fuel Consumption | 395 g/min |
| Maximum Allowable Exhaust Temperature | 700 ℃ |
| Ignition Mode | Full Automatic Fuel Ignition |
| Compatible Civilian Fuels | Aviation Kerosene, Diesel, General Civilian Gasoline |
| Engine Type | Micro Turbojet UAV Gasoline Engine |
| Main Application | Civilian high-speed fixed-wing UAV, Aerial survey drone, Large RC aircraft |
Detailed Structural & Technical Features
Automatic Fuel Ignition Startup System
This UAV gasoline engine removes manual startup mechanisms, adopting fully integrated automatic fuel ignition control module. The ECU automatically adjusts fuel supply and ignition timing according to ambient temperature and altitude, realizing fast, reliable cold start even in low-temperature mountain and high-altitude environments. Short startup time reduces ground preparation work for civilian drone operators.
Leak-Proof Sealing & Low-Loss Lubrication Structure
Exclusive multi-layer composite sealing ring design eliminates lubricant dripping at low initial RPM, a widespread flaw of ordinary micro turbojet UAV engines. The optimized bearing lubrication system only requires a 2% oil mixing ratio for repeated flight missions, cutting lubricant purchasing costs and reducing carbon accumulation inside the turbine chamber. For single-shot short-duration test flights, extra lubricant mixing is unnecessary.
High-Efficiency Fuel Atomization & Full Combustion Assembly
Built-in proprietary fuel mixing nozzle improves fuel atomization uniformity under different pressure conditions. Full fuel combustion lowers residual exhaust emissions and reduces overall fuel consumption per flight hour, meeting global civilian aviation environmental standards. Stable atomization performance avoids flameout risks during rapid throttle adjustment for high-speed civilian drone flight.
Reinforced Anti-Vibration & Corrosion-Resistant Overall Frame
All fasteners use anti-loosening vibration-resistant locking design, paired with surface salt-fog resistant coating on the engine shell. The whole unit can maintain stable operation under strong airflow vibration, coastal high-humidity and dusty field environments. The streamlined body layout reduces flight wind resistance, further boosting the effective flight range of civilian UAV platforms.
High-Speed Balanced Rotor & Low-Temperature Cooling Technology
Precision dynamic balancing processing eliminates rotor unbalance vibration under ultra-high 115000 RPM operation. Independent circulating cooling channel surrounds bearings and rotor shafts to control core component temperature far below the industry average, directly extending the overhaul cycle and total service life of this drone gasoline engine.
Civilian Commercial Application Scenarios
This micro turbojet UAV engine is only applicable to non-military civilian industrial and recreational aviation fields:
- High-speed aerial survey & mapping: Long-distance terrain scanning, highway high-speed inspection, mountain resource monitoring
- Commercial aerial filming: Ultra-fast panoramic landscape shooting, large venue aerial recording
- Civilian environmental monitoring: River basin full-range patrol, forest large-area vegetation observation
- Educational aviation research: University aerospace lab test platforms, civilian aviation training models
- Large high-speed RC fixed-wing aircraft for hobby and commercial exhibition
Packaging & Global Shipping
Standard Export Packing: Custom shock-resistant aluminum alloy inner box + reinforced fumigated wooden outer case, with temperature-insulated foam lining to protect precision turbine components during cross-border transport.
Supported International Trade Terms: EXW, FOB, CIF, DDP and door-to-door global delivery cooperation with worldwide professional aerospace freight providers.
Customized Packing Service: Separate anti-rust oil wrapping for all rotating core parts available for bulk wholesale orders.
Delivery Lead Time: Single sample unit shipped within 10 working days; mass bulk production orders delivered within 20–25 working days after deposit confirmation.
Factory Production & Strict Quality Control
Every finished micro turbojet UAV gasoline engine undergoes 5 major inspection links before delivery:
- Raw material incoming test for high-temperature alloy rotor, sealing parts and ECU electronic control components.
- Ultra-high-speed rotor dynamic balancing calibration and vibration value detection.
- Full-throttle continuous 2-hour bench test, real-time recording thrust, RPM, fuel consumption and exhaust temperature data.
- Sealing leak test and low-temperature cold start simulation test for high-altitude environments.
- Complete assembly appearance inspection and anti-rust protective treatment before packaging.
Each drone gasoline engine carries an independent unique serial number, with all bench test data permanently archived to provide traceable quality assurance for global civilian UAV integrators.
Frequently Asked Questions
FAQ 1: What civilian fuels can be used for this 130N micro turbojet UAV engine? Are there any fuel usage restrictions?
Answer: This UAV gasoline engine supports civilian aviation kerosene, standard diesel and common civilian gasoline. Ethanol-blended fuel with ethanol content over 10% is prohibited, as ethanol will cause severe carbon accumulation inside the turbine chamber and block the precision atomization nozzle. Always filter fuel before adding it to the engine fuel tank to avoid particle blockage of the fuel supply pipeline. Follow the 2% lubricant mixing ratio for repeated long-duration flight missions.
FAQ 2: Can this turbojet drone gasoline engine be installed on hybrid VTOL civilian UAVs? What maintenance cycles should users follow?
Answer: This UAV engine is mainly optimized for high-speed fixed-wing civilian drones; it can be matched with large hybrid VTOL platforms after consulting our technical team for airframe structural reinforcement plans. Standard maintenance cycle: full disassembly inspection every 50 flight hours, replacing sealing rings and lubrication pipelines. The rotor and cooling structure only need routine cleaning after every 10 flight hours to maintain stable thrust output and extend engine service life.
Inquiry & Cooperation Guide
If you need sample bench testing, bulk wholesale quotation, airframe matching technical consultation, installation operation manuals or flight parameter tuning documents for this 130N micro turbojet UAV gasoline engine, please submit your inquiry via the website contact form or official business email. Our professional aerospace power technical sales team will reply to all consultation requests within 24 working hours and provide free global civilian UAV after-sales service policy documents.
