DLA 116CC HF TWIN Cylinder UAV Engine

The data is just of a random engine we test, which is for reference only. In actual use, the data will fluctuate due to the influence of environmental temperature, altitude, carburetor/electric injection adjustment method and different brand propellers. Please be noted.

Advantage?

1. With cowling, airflow rectifier and heat preservation at high altitude.

2. EFI system, suitable for high altitude flying.

3. Double spark plug design, better reliability andstability.

4. The cylinder head is splited and machined by CNC, the engineruns more consistently.

5. Cylinder equipped with pressure reducing valve, it makeengine start easier.

6. Electrical parts with aviation plugs, more solid andreliable.

7. Improved material and machining technology.

What is the difference in between hobby engine & UAV engine

UAV engine is designed for industrial use and long endurance. The materials used for UAV engine shaft/piston ring etc are all in A grade material in order to achieve the performance.

All the UAV engines with all in one (Generator/autostarter) only for pre-order. Production time nromally takes 10-30 days. TEAMAUSTARS Provide 24/7 technical support online with WhatsApp +610433000015

DLA 180i2 CC PETROL ENGINE NOW RELEASED!

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BO 50-100HOURS

BO 50-100HOURS

All the UAV engines with all in one (Generator/autostarter) only for pre-order. Production time nromally takes 10-30 days. TEAMAUSTARS Provide 24/7 technical support online with WhatsApp +610433000015

Displacement: 116cc

Engine weight: 4060g

Idle speed: 2500rpm

Starting power supply voltage: 12S lithium battery

Cylinder bore*stroke: 46mm*35mm

Compression ratio: 8:1

Maximum fuel consumption: 2.85L/h

Spark plug: Iridium spark plug*2

Power generation system: Controller: 605g

Self-start function: yes

Lubrication ratio: 50:1

Fuel/lubricant: aviation kerosene/fully synthetic two-stroke motor oil

Advantage:

1. Can be customized according to customer requirements.

2. Stable performance; easy to use; long service life; strong power; stable rapid acceleration performance; simple and compact structure, small size, convenient maintenance. Applicable altitude is below 4000m.

Precautions:

1. Please use the mill oil specified by the manufacturer

2. The lubrication ratio during grinding is 20:1, and the grinding time is 2-3 hours.

3. Do not disassemble or install the engine without authorization. If you need to disassemble and install, you must contact the manufacturer and proceed under the manufacturer's guidance.

4. The ground test needs to install an air filter; pay attention to prevent dust and impurities from being sucked into the carburetor.

5. It is forbidden to adjust the mixing ratio screw casually. If you need to adjust, please contact the manufacturer.

6.The picture is for reference only.

BO 50-100HOURS

What is the difference in between hobby engine & UAV engine

UAV engine is designed for industrial use and long endurance. The materials used for UAV engine shaft/piston ring etc are all in A grade material in order to achieve the performance.

All the UAV engines with all in one (Generator/autostarter) only for pre-order. Production time nromally takes 10-30 days. TEAMAUSTARS Provide 24/7 technical support online with WhatsApp +610433000015

DLA 180cc HF UAV/UAS Engine 2021 Version

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BO 50-100HOURS

What is the difference in between hobby engine & UAV engine

UAV engine is designed for industrial use and long endurance. The materials used for UAV engine shaft/piston ring etc are all in A grade material in order to achieve the performance.

All the UAV engines with all in one (Generator/autostarter) only for pre-order. Production time nromally takes 10-30 days. TEAMAUSTARS Provide 24/7 technical support online with WhatsApp +610433000015

Engine:DLA720

Exhaust:720 cm³?43.9 inch³?

Cylinder:4 Cylinders

Displacement:Horizontal

Cooling :Air

Exhaust bore:65mm(2.5 inch)

Cylinder work temperature?80~120°C

Stroke:54mm(2.12 inch)

Power:60HP at 6000rpm

Weight:≈22Kg(engine body)

RPM:2000-6600 rpm (It is better less than 6000rpm)

Start method:Self - Starting

Thrust:95Kg (attitude=100m)

Recommend propeller:38*14 ?40*16

Spark plug:DLA CM6(Two Iridium)

Compression Ratio:8.6:1

Fuel:95# gasoline(GB17930-2006), mixed with 2T fully synthetic oil

Lubrication Ratio: 15:1(Trial Run) 20:1(Normally Flying)

BO 50-100HOURS

This engine is mainly used for fixed-wing with take-off weights (including Gasoline) not more than 12 KGS. Its crankcase, crankshaft, central screws are all made of domestic high-performance materials by CNC processing method. With beautiful appearance, high-precision, drop resistance, fatigue resistance, good stability, strong power performance, we get good reputations from plane enthusiasts after more than 4 years continuously upgrade. Our company will be grateful for your valuable guidance and advice!!

What is the difference in between hobby engine & UAV engine

UAV engine is designed for industrial use and long endurance. The materials used for UAV engine shaft/piston ring etc are all in A grade material in order to achieve the performance.

All the UAV engines with all in one (Generator/autostarter) only for pre-order. Production time nromally takes 10-30 days. TEAMAUSTARS Provide 24/7 technical support online with WhatsApp +610433000015

One key start, dc power generation;

Starting input voltage 24V, 28V optional,

power generation output power 400W, 600W optional;

32cc , 58cc , 64cc , 116cc and 180cc, various types of optional;

Accept professional custom, welcome to call or email consultation!

NEW PRODUCT 2023 WITH ONE KEY STARTER/GENERATOR 28V/1200W/2000W/3000W/6000W Options. The base price is for the version with 28V/1200W One key starter

New version less 2.5kg weight (One key starter/generator vs Electric starter+Generator/Magnetic version)

LIMBACH L550 EF-G Engine (2-4 weeks testing and Ready TO Ship)

Ignition Leads=Shielded Ignition Leads

Al coupling=Alternator/Generator coupling Kit

We are one of the authorised dealers to supply all Limbach engines and parts to worldwide. For these countries where local dealers are capable of supplying the engine, we recommend customers to contact them. If not, we can help!

"L 550 EF-G" - 37 kW

Four cylinder, horizontally opposed, air cooled, two cycle engine, with electronic engine management system and mixture lubrication. NEW PRODUCTION 2023 LESS WEIGHT 2.5kg comparing normal version (electric starter+generator)

LIMBACH L550 E Engine (5-6 weeks testing and Ready TO Ship)

Generator/Alternator: 14V 1200W or 28V 1200W Optional

Ignition Leads=Shielded Ignition Leads

Al coupling=Alternator/Generator coupling Kit

"L 550E" - 37 kW

Four-cylinder, two-stroke boxer engine, air cooling, single magneto ignition, 4 carburettors, mixture lubrication

Four cylinder, horizontally opposed, air cooled, two cycle engine, with solid state magneto ignition, mixture lubrication. Suitable for pusher and tractor installations.

Performance .............................................................. 37 kW (50 HP) at 7500 rpm
Bore .......................................................................................... 66 mm / 2.60 inch
Stroke ....................................................................................... 40 mm / 1.57 inch
Displacement ............................................................. 548 cm3/ 33.44 cub. inches
Crankcase .................................................................................. Aluminum casting
Crankshaft ..................................................................... Drop forged, seven piece
Pistons .......................................................... Cam ground, casted aluminum alloy
Cylinders ........................................ Casted aluminum alloy, with Ceramic coating
Ignition system ........................................................ Solid state magneto ignition
Firing Order ................... Two opposing cylinders simultaneously, 180 deg. offset
Carburetors ................................................. 4 diaphragm all position carburetors
Starter ............................................................................................. 12V (+4.0 kg) Optional
Generator ......................................................................................... 28 V 1200 W Optional
Dry weight approx ....................................................................................... 16 kg
Fuel: AVGAS 100LL or 90 RON mixed with a suitable oil to the ratio of 1:25 or 1:50 (with synthetic oil)
Spark Plug ........................................................................... 4 pcs ( Bosch WS5F )Exhaust Stacks ....................................................................... 120 mm or 150 mm

Propeller .................................................................................................... 30 - 25

Cylinders with additional heat sinks .......................................................... 1.2 kg Optional

ONE KEY STARTER version includes complete engine with air/fuel filters, fuel pump/harness cables, PMU (POWER MANAGEMENT UNIT) FOR AC-DC, ignition leads, suspension cushion pad. To compare the old version with magnetic starter and the version with starter/generator, one key starter version has the less weight and more efficiency for the performance.

LIMBACH L275EF Engine (2-3 weeks testing and Ready TO Ship)

Generator/Alternator: 28V 1000W standard, 2000W, 3000W Optional

Ignition Leads=Shielded Ignition Leads

Al coupling=Alternator/Generator coupling Kit

Muffler stacks/2pc (optional)

"L 275 EF" - 18 kW

Two cylinder, horizontal opposed, air cooled, two cycle engine, with fuel saving electronic engine management system and mixture lubrication.

LIMBACH L275E Engine (5-6 weeks testing and Ready TO Ship)

Generator/Alternator: 14V 1200W or 28V 1200W Optional

Ignition Leads=Shielded Ignition Leads

Al coupling=Alternator/Generator coupling Kit

L 275E" - 15 kW

Two-cylinder, two-stroke boxer engine, air cooling, single magneto ignition, 2 carburettors, mixture lubrication

Two cylinder, horizontally opposed, air cooled, two cycle engine, with solid state magneto or battery ignition, mixture lubrication. Suitable for pusher and tractor installations.

Performance .............................................................. 15 kW (20 HP) at 7200 rpm
Bore .......................................................................................... 66 mm / 2.60 inch
Stroke ....................................................................................... 40 mm / 1.57 inch
Displacement ............................................................. 274 cm3/ 16.72 cub. inches
Crankcase .................................................................................. Aluminum casting
Crankshaft ....................... Drop forged, one piece utilizing 2 split connecting rods
Pistons .......................................................... Cam ground, casted aluminum alloy
Cylinders ........................................ Casted aluminum alloy, with Ceramic coating
Ignition system ........................................................ Solid state magneto ignition
Firing Order ........................................................... Both cylinders simultaneously
Carburetors ......................... 2 diaphragm all position carburetors, without choke
Starter .............................................................................................. 12 V, 0.3 kW (Optional)
Generator ........................................................................................ 28 V, 1200 W (Optional)
Dry weight approx .................................................. 7.2 kg with magneto ignition
Fuel ....................................................................... AVGAS 100LL or 90 RON mixed
Optional Equipment ..................... Cylinders with additional heat sinks (+ 0.6 kg) (Optional)
Shielded ignition system, Long and short crankshafts, Exhaust stacks

* Two cylinders horizontally opposed; (ENGINE TESTED AND APPROVED BY APOLLO-45G VTOL drone to achieve over 20 Hours endurance)

* Two strokes;

* Air cooling;

* Dual redunDant speed sensor;

* electronic closed-loop control;

* Optional One Key Starter/generator;

* Own IP development of engine, ECU and fuel pump; (not select the after market one)

* Better environmental adaptability;

* Lower specific fuel consumption to meet the needs of long endurance;

* Engine thermal management technology to ensure engine stability and long TBOH

* The engine body is always in an appropriate temperature range with integrated cooling mounting ;

* Easier to use;

* Higher durability reliability;

24/7 Technical support by teamaustars for protocol integration and support

Model number :B2H170

Displacement :170cc

Maximum power :15HP

The rotational speed ranges from 1800 to 8000rpm

Applicable fuel: jet coal RP-3

Minimum specific fuel consumption: 388g/kwh

Fuel system: Electronic control

Ignition system: Electronic control

Lubrication mode: mixed lubrication of fuel oil and lubricating oil, lubricating oil/fuel oil ratio: 1:50

Cooling method: Air cooling

Throttle control mode: throttle electronic control

Applicable temperature :-30 Celsius ~+55 Celsius

Starting altitude 4000 meters

Output axis rotation: counterclockwise (from the end of the output axis)

Weight composition

Engine body :5337 g

ECU: 169 g

Fuel pump :213 g

CDI :175 g

Wiring harness :200 g

Exterior dimension

Length x width x height: 265 x 371.1 x 273.4

Other configurations are optional

Damping system

Inspired integrated configuration/generator configuration

Recommended propeller specification

Two blades: 26x18, 28x16, 28x14, 30x12, 30x10

Three-blade paddle: 24x18, 24x16, 25x12, 25x14

System overview
The DLE60 EFI provides drones with increased reliability and power while addressing the shortcomings commonly found in two-stroke engines.

This integrated design features a coaxial starter/generator unit with no gear connection. It outputs 24V and has a power of 260W, which can meet the power requirements of onboard equipment for fixed-wing drones.

The newly designed fuel pump, with self-priming capability, adopts closed-loop pressure control to precisely control the fuel pressure without returning to the fuel tank. The DLE60 EFI incorporates the latest engine technology from LUTAN EFI and DLE Engine. Provide RS232 communication protocol to obtain engine running data in real time.

Engine package includes:
EFI ECU
Self-priming fuel pump
24V Starter-Regulator Module
wiring harness
CDI module
Isolation Rack

Power: 7HP/8500rpm(*The data comes from the official DLE source.)
Static thrust: 15.2kg/100m height(*The data comes from the official DLE source.)
Static thrust: 13.5kg/1800m height(*The data comes from the official DLE source.)
Recommended propellers: 22x8; 22x10; 23x8; 23x10;
Displacement: 61cm3
Lubrication ratio: 40:1
Weight (engine with air intake): 2.51kg
Weight (starter/generator unit): 420g
Weight (ECU): 110g
Weight (fuel pump): 165g
Voltage: 12V
Power Draw: 1 Amp peak, 1 hour / 1,000mAh
Temperature range: -20° – 50° C

NEW PRODUCT 2024, LESS 3 KG WEIGHT VS OLD VERSION

Weight for NEW VERSION ENGINE (ALL IN ONE) 16KG PRICE FOR EXPORT W/O TAX $29000 USD PLUS FREIGHT $350 USD, FOR LOCAL W/TAX GST 10% PRICE IS $31000 USD

Weight for OLD VERSION ENGINE (ALL IN ONE) 19KG

Product Description

Specifications

Engine Type ............................................................... Single rotor Wankel-type spark ignition engine
Capacity .................................................................................................................. 208 CC chamber size
Power Output ............................................................................................ 38 bhp ( 28 kw ) at 7800 rpm
Weight ...............................................................................................................................
Specific Fuel Consumption .......................... 0.57 Ib/bhp/hr at max power, 0.52 Ib/bhp/hr at cruise
Vibration Levels ..................................................................................... Nominally Zero radial vibration
Housing Cooling ............................................................................................................................ Ram Air
Rotor Cooling .................................................................................................................................. Ram Air
Cylinders ...................................................................... Casted aluminum alloy, with Ceramic coating
Direction of Rotation .............................................. Anti - Clockwise, Viewed on propeller mounting
Ignition System ................................................................................... Electronic contact-less magneto
Carburettors ..................................... Diaphragm - type with integrated pressure - pulse fuel pump
Fuel Type ............................................................................. Mogas Regular grade or AVGAS ( 100 LL )
Lubrication ...................................... Via fixed - flow oil metering pump supplied from separate tank
Spark Plug ................................................................................................................ 2 pcs ( NGK CR9EK )
Generator ............................................................................................................................. 28 V 850 Watt
Propeller ........................................................................................................................................... 28 - 20

TBOH: 70-100

The 68CC Engine is an air cooled horizontally opposed piston engine with electronically controlled fuel injection. Compared with its counterparts in the market, the engine is light weighted, consistent in performance, robust and maintenance friendly. 68CC is an ideal choice to power fixed-wing UAV and VTOL of MTOW 25kg-35kg.

TEAM AUSTARS PROVIDE 24/7 TECHNICAL SUPPORT AND PROTOCOL INTEGRATION BY WHATSAPP ONLINE

PRODUCT&PERFORMANCE APPROVED BY TEAM AUSTARS

PRICE SHARPLY WAS DROPPED DUE TO MASS PRODUCTION AND MARKET DEMAND!

Technical Parameter

The 312CC engine is an air cooled horizontally opposed piston engine with dual-redundant TCI ignition. Compared with its counterparts in the market,the engine is light weighted, consistent in performance, robust and maintenance friendly. 312CC is an ideal choice to power fixed-wing UAV and VTOL of MTOW 140kg~ 200kg. FOR PROTOCOL INTEGRATION, CONTACT TEAM AUSTARS TO GET 24/7 TECHNICAL SUPPORT

THIS IS HEAVY FUEL VERSION

PRICE SHARPLY WAS DROPPED DUE TO MASS PRODUCTION AND MARKET DEMAND! THIS ENGINE IS UNDER EXPORT CONTROL

Technical Parameter

Configuration	2Cyl. Horizontally Opposed	Displacement	312ml
Bore × Stroke	65mm×47mm	Speed Range	1600rpm~7000rpm
Compression Ratio		10.6:1
Lubrication	Oil Gas Lubrication	Fuel Delivery	Electronic Fuel Injection
Fuel Type	3# JET Fuel (or 92# Gasoline and Above, Aviation Gasoline)
Starting Method	External Starter Starting, Integrated Starter Starting
Starting Conditions	Cylinder Temperature ≥ 85 Celsius (JET Fuel),Throttle Position ≥ 25%
Weight	10.8kg	Fuel Consumption	410g/kW·h
Rated Power	18.4kW@8000rpm	Generator	Customized

The 183CC engine is an air cooled horizontally opposed piston engine with dual- redundant TCI ignition. Compared with its counterparts in the market,the engine is light weighted, consistent in performance, robust and maintenance friendly. 183CC is an ideal choice to power fixed-wing UAV and VTOL of MTOW 60kg~120kg

TEAM AUSTARS PROVIDE 24/7 TECHNICAL SUPPORT WITH COM/PROTOCOL FOR AUTOPILOT INTEGRATION. FREE CUSTOMISED ENGINE MOUNTING FRAME TO FIT EACH PROJECT

PRICE SHARPLY WAS DROPPED DUE TO MASS PRODUCTION AND MARKET DEMAND!

Technical Parameter

The 68CC Engine is an air cooled horizontally opposed piston engine with electronically controlled fuel injection. Compared with its counterparts in the market, the engine is light weighted, consistent in performance, robust and maintenance friendly. 68CC is an ideal choice to power fixed-wing UAV and VTOL of MTOW 25kg-35kg.

Package includes: 1 x complete engine with mufflers, CDI etc + auto starter + Protocol converter for PIXHAWK

PRICE SHARPLY WAS DROPPED DUE TO MASS PRODUCTION AND MARKET DEMAND!

Technical Parameter

The 68CC Engine is an air cooled horizontally opposed piston engine with electronically controlled fuel injection. Compared with its counterparts in the market, the engine is light weighted, consistent in performance, robust and maintenance friendly. 68CC is an ideal choice to power fixed-wing UAV and VTOL of MTOW 25kg-35kg.

Package includes complete EFI engine with FUEL PUMP, EMU etc + Communication protocol converter for Pixhawk

PRICE SHARPLY WAS DROPPED DUE TO MASS PRODUCTION AND MARKET DEMAND!

Technical Parameter

The 312CC engine is an air cooled horizontally opposed piston engine with dual-redundant TCI ignition. Compared with its counterparts in the market,the engine is light weighted, consistent in performance, robust and maintenance friendly. 312CC is an ideal choice to power fixed-wing UAV and VTOL of MTOW 140kg~ 200kg.

PRICE SHARPLY WAS DROPPED DUE TO MASS PRODUCTION AND MARKET DEMAND! THIS ENGINE IS UNDER EXPORT CONTROL

Technical Parameter

Configuration	2Cyl. Horizontally Opposed	Displacement	312ml
Bore × Stroke	65mm×47mm	Speed Range	1600rpm~7000rpm
Compression Ratio		10.6:1
Lubrication	Oil Gas Lubrication	Fuel Delivery	Electronic Fuel Injection
Fuel Type	3# JET Fuel (or 92# Gasoline and Above, Aviation Gasoline)
Starting Method	External Starter Starting, Integrated Starter Starting
Starting Conditions	Cylinder Temperature ≥ 85 Celsius (JET Fuel),Throttle Position ≥ 25%
Weight	10.8kg	Fuel Consumption	410g/kW·h
Rated Power	18.4kW@6700rpm	Generator	Customized

The 183CC engine is an air cooled horizontally opposed piston engine with dual- redundant TCI ignition. Compared with its counterparts in the market,the engine is light weighted, consistent in performance, robust and maintenance friendly. 183CC is an ideal choice to power fixed-wing UAV and VTOL of MTOW 60kg~120kg.

TEAM AUSTARS PROVIDE 24/7 TECHNICAL SUPPORT WITH COM/PROTOCOL FOR AUTOPILOT INTEGRATION. FREE CUSTOMISED ENGINE MOUNTING FRAME TO FIT EACH PROJECT.

PRICE SHARPLY WAS DROPPED DUE TO MASS PRODUCTION AND MARKET DEMAND!

Technical Parameter

The 312CC engine is an air cooled horizontally opposed piston engine with dual-redundant TCI ignition. Compared with its counterparts in the market,the engine is light weighted, consistent in performance, robust and maintenance friendly. 312CC is an ideal choice to power fixed-wing UAV and VTOL of MTOW 120kg~ 200kg.

FOR PROTOCOL INTEGRATION, CONTACT TEAM AUSTARS TO GET 24/7 TECHNICAL SUPPORT BY WHATSAPP

PRICE SHARPLY WAS DROPPED DUE TO MASS PRODUCTION AND MARKET DEMAND! THIS ENGINE IS UNDER EXPORT CONTROL

Technical Parameter

Configuration	2Cyl. Horizontally Opposed	Displacement	312ml
Bore × Stroke	65mm×47mm	Speed Range	1600rpm~7000rpm
Compression Ratio		10.6:1
Lubrication	Oil Gas Lubrication	Fuel Delivery	Electronic Fuel Injection
Fuel Type	3# JET Fuel (or 92# Gasoline and Above, Aviation Gasoline)
Starting Method	External Starter Starting, Integrated Starter Starting
Starting Conditions	Cylinder Temperature ≥ 85 Celsius (JET Fuel),Throttle Position ≥ 25%
Weight	10.8kg	Fuel Consumption	410g/kW·h
Rated Power	18.4kW@6700rpm	Generator	Customized

Features:

1. More Fuel Efficient: Reed valve dual intake (vs. piston valve/4-carb) reduces fuel consumption. Max consumption: 18-19L/hr (vs. other brands's ~23-24L/hr). 20% fuel saving comparing Carburettor version
2. Easier Tuning & Optimal Performance: Dual carburetors are simpler to synchronize than four carby Each engine is factory-calibrated using instruments, with test records, ensuring perfect air-fuel ratio and combustion efficiency.
3. Simpler & More Reliable: Streamlined design eliminates complex 4-carby linkage, improving reliability. Long lasting by ceramic coat for inner cylinders
4. Optional Heater for easy start in extreme cold winter.
5. Powerful Starter: High-power starter motor for effortless starting.
6. Optional Compact Generator: Lightweight, stable 28V 500W/1000W/2000W generator & PSU provides continuous power for aircraft/equipment.
7. Optional Prop/engine Brake: Enhances parachute deployment success in pusher UAVs by stopping the propeller beforehand.

• 8. Rigorous QC & Traceability: All critical components undergo factory testing with records archived, ensuring quality and traceability.
• 9. Pre-Broken In: Engines are factory run-in, ready for immediate use.
• 10. Support customised configurations (exhaust direction, rotation CW/CCW)

TBO>300H warranty 100Hours or 1 Year

Parameter:

Engine type: two-stroke four-cylinder

Speed range: 1500-7200rpm

Cooling type: natural air cooling

Rotation direction: clockwise facing the propeller CW or CCW

Weight: 20.8kg (including starter)

Generator: 28V 500W, 1000W, 2000W (optional)

Size: 350mm* 450mm* 240mm(L*W*H)

Maximum power: 40kw/7200rpm

Fuel: 92-95 gasoline, 40:1 fully synthetic lubricant

Ignition system: DC CDI electronic ignition

Propeller: 28*24-34*18

Features:

*The JIN-342 engine uses a horizontally opposed twin-cylinder

*Aluminum alloy casting piston, light weight and high power

*High performance pump membrane carburetor

*Fuel: Gasoline

*DC CDI ignition system

*The clutch can be installed at the front of the engine

*The starter can be installed on the fuselage

*The engine can be equipped with various generators such as 500W, 1000W, 2000W, etc.

Parameter:

Engine type: two-stroke twin cylinder

Speed range: 1500-7000rpm

Cooling type: natural air cooling

Rotation direction: counterclockwise facing the propeller

Weight: 10.5kg

Generator: 28V, 500W, 1000W

Dimensions: 310mm* 400mm* 330mm(L*W*H)

Maximum power: 18kw/7500rpm

Fuel: 92-95 gasoline, 40:1 fully synthetic lubricant

Ignition system: DC CDI electronic ignition

Propeller: 30*20-36*14

Features:

1.Twin cylinder single intake design with ceramic coated inner cylinders;

2.Aluminum alloy casting piston;

3.High performance pump membrane carburetor;

4.DC CDI ignition system;

5.Various engine output connection forms;

6.Comes with throttle servo bracket;

7.The JIN-183CC EFI engine can be adapted to different types of propellers;

8.The engine can be equipped with various generators.

TBO>300H, 100 Hours / 1 Year Waranty

Parameter:

Engine type: two-stroke twin cylinder

Speed range: 1800-7000rpm

Cooling type: natural air cooling

Rotation direction: clockwise or counterclockwise adjustable at any time

Weight: 4500g

Maximum power: 11KW/6500rpm

Fuel: 92-95# gasoline, 40:1 fully synthetic lubricant

Ignition system: DC CDI electronic ignition

Dimensions: 210mm*330mm*160mm (L*W*H)

Propeller: 24*16-28*10

The JIN-250SA engine is a two-stroke horizontally opposed twin-cylinder, water-cooled aircraft engine. The engine displacement is 248cc and the maximum power is 21hp.

Features:

1.Water cooling;

2.Integral cylinder crankcase;

3.Cylinder and cylinder block ceramic plating technology, forged crankshaft, high-strength piston

4.DC automatic timing CDI ignition system;

5.Built-in electric starter, one-button starting.

6.The JIN-250SA engine can be adapted to different types of propellers from 32 to 36 inches.

Parameter:

Engine type: two-stroke twin cylinder

Speed range: 1500-7000rpm

Cooling type: natural air cooling

Rotation direction: clockwise facing the propeller

Weight: 12.5kg

Generator: 14V 300W

Size: 210mm * 330mm * 160mm(L*W*H)

Maximum power: 15.5kw/7500rpm

Fuel: 92-95 gasoline, 40:1 fully synthetic lubricant

Ignition system: DC CDI electronic ignition

Propeller: 29*20, 30*18, 32*16

Features:

1.Twin cylinder single intake design with ceramic coated inner cylinders;

2.Aluminum Alloy Piston;

3.High performance pump membrane carburetor;

4.Fuel: Gasoline;

5.DC CDI ignition system;

6.Various engine output connection forms;

7.Comes with throttle servo bracket;

8.The JIN-183CC engine can be adapted to different types of propellers;

9.The engine can be equipped with various generators.

TBO>300H 100Hours/1 Year warranty

Parameter:

Engine type: two-stroke twin cylinder

Speed range: 1800-7000rpm

Cooling type: natural air cooling

Rotation direction: clockwise or counterclockwise adjustable at any time or CW CCW optional

Weight: 4500g

Maximum power: 11KW/6500rpm

Fuel: 92-95# gasoline, 40:1 fully synthetic lubricant

Ignition system: DC CDI electronic ignition

Dimensions: 210mm*330mm*160mm(L*W*H)

Propeller: 24*16-28*10

Features:

1.Twin cylinder single intake design;

2.Aluminum alloy casting piston;

3.High performance pump membrane carburetor;

4.Fuel: Gasoline;

5.DC CDI ignition system;

6.Different power outputs can be selected: clutch, reduction box, brake, etc;

7.Optional electric starter;

8.The JIN-274CC engine can be adapted to different types of propellers ranging from 30 to 34 inches.

9.The engine can be equipped with various generators.

Parameter:

Engine type: two-stroke twin cylinder with ceramic coat inner cylinder, coated piston for long lasting

Speed range: 1500-7500rpm

Cooling type: natural air cooling

Rotation direction: counterclockwise facing the propeller

Dimensions: 210mm*330mm*160mm(L*W*H)

Generator: 14V 300W or 28V 600W (optional)

Weight: 7400g

Maximum power: 16kw/7200rpm

Fuel: 92-95 gasoline, 40:1 fully synthetic lubricant

Ignition system: DC CDI electronic ignition

Propeller: 32*18-34*16

TBO>300H 100Hours / 1 Year factory warranty

Features:

1.Electronic fuel injection system with ceramic coated inner cylinders, forged crankshaft, aluminim fabricated piston for long lasting

2.Horizontally opposed twin cylinder design;

3.Aluminum alloy casting piston;

4.Fuel: Gasoline;

5.DC CDI ignition system;

6.Different power outputs can be selected: clutch, reduction box, brake, etc;

7.Optional electric starter;

8.The JIN-275CC EFI engine can be adapted to different types of propellers ranging from 30 to 34 inches;

9.The engine can be equipped with various generators

Parameter:

Engine type: two-stroke twin cylinder

Speed range: 1500-7500rpm

Cooling type: natural air cooling

Rotation direction: counterclockwise facing the propeller

Dimensions: 210mm*330mm*160mm(L*W*H)

Generator: 14V 300W or 28V 600W (optional)

Weight: 10800g (including ECU and starter)

Maximum power: 16kw/7500rpm

Fuel: 92-95 gasoline, 40:1 fully synthetic lubricant

Ignition system: DC CDI electronic ignition

Propeller: 28x24-34x18

Autostarter: 12V/400w

Features:

1.The engine adopts a four-cylinder dual-intake design;

2.Aluminum alloy casting piston, light weight and high power;

3.High performance pump membrane carburetor;

4.Fuel: Gasoline;

5.DC CDI ignition system;

6.Provides a variety of engine output connection forms;

7.The starter can be installed on the fuselage;

8.The JIN-550CC engine can be adapted to different types of propellers ranging from 32 to 34 inches

TBO>300H, 100 Hours/1 x Year warranty

Parameter:

Engine type: two-stroke four-cylinder

Speed range: 1500-7500rpm

Cooling type: natural air cooling

Rotation direction: clockwise facing the propeller

Weight: 19.7kg (including starter)

Generator: 14V 300W or 28V 600W (optional)

Dimensions: 350mm * 450mm * 240mm(L*W*H)

Maximum power: 40kw@7500rpm

Fuel: 92-95 gasoline, 40:1 fully synthetic lubricant

Ignition system: DC CDI electronic ignition

Propeller: 28*24-34*18

Features:

1.The engine adopts a four-cylinder dual-intake design;

2.Forged crankshaft, cast piston;

3.Electronic fuel injection system;

4.Fuel: Gasoline;

5.DC CDI ignition system;

6.The starter can be installed on the fuselage;

7.The starter can be installed on the fuselage;

8.Optional various generators;

9.The JIN-550EFI engine can be adapted to different types of propellers ranging from 32 to 34 inches.

TBO>300H 100 Hours/1 x Year Warranty

Parameter:

Engine type: two-stroke four-cylinder

Speed range: 1500-7500rpm

Cooling type: natural air cooling

Rotation direction: clockwise facing the propeller

Weight: 20.8kg (including starter)

Generator: 14V 300W or 28V 600W (optional)

Size: 350mm* 450mm* 240mm(L*W*H)

Maximum power: 37kw/7500rpm

Fuel: 92-95 gasoline, 40:1 fully synthetic lubricant

Ignition system: DC CDI electronic ignition

Propeller: 28*24-34*18

Customised engine starter for MDR208PRO by Teamaustars

• Over-run clutch for positive drive applications
• Heavy-duty cable and battery connectors
• Heavy Duty Starter CW Engine Rotation (sitting behind watching )
• 
  
• 
  
• Torque: 10+ Nm
• Max RPM: 2000
• Peak Power: 2.6 KW
• Supply: 12V/500A
• Dimension: 500mm x 280mm x 140mm
• Weight: 5.4 KG
• Wire Length: 2 m
• Connectors: 2x battery terminal connectors

Product Description

Specifications

Engine Type ............................................................... Single rotor Wankel-type spark ignition engine
Capacity .................................................................................................................. 208 CC chamber size
Power Output ............................................................................................ 38 bhp ( 28 kw ) at 7800 rpm
Weight ...............................................................................................................................
Specific Fuel Consumption .......................... 0.57 Ib/bhp/hr at max power, 0.52 Ib/bhp/hr at cruise
Vibration Levels ..................................................................................... Nominally Zero radial vibration
Housing Cooling ............................................................................................................................ Ram Air
Rotor Cooling .................................................................................................................................. Ram Air
Cylinders ...................................................................... Casted aluminum alloy, with Ceramic coating
Direction of Rotation .............................................. Anti - Clockwise, Viewed on propeller mounting
Ignition System ................................................................................... Electronic contact-less magneto
Carburettors ..................................... Diaphragm - type with integrated pressure - pulse fuel pump
Fuel Type ............................................................................. Mogas Regular grade or AVGAS ( 100 LL )
Lubrication ...................................... Via fixed - flow oil metering pump supplied from separate tank
Spark Plug ................................................................................................................ 2 pcs ( NGK CR9EK )
Generator ............................................................................................................................. 28 V 850 Watt
Propeller ........................................................................................................................................... 28 - 20

TBOH: 70-100

The DLE30RA EFI engine adopts a single-cylinder side exhaust design, which is suitable for various small drones.

The full set of engines includes:

LUTAN EFI ECUs

Fuel pump

required wiring harness

CDI module

mounting standoffs

Power: 3.7HP/8500rpm

Thrust: 8.5kg/Sea Level/100M

Thrust: 7.5kg/Sea Level/1800M

Props Range: 18x8;18x10;19x8;20x8

CC: 30.5cm3

Mix: 30:1

Engine weight: 920g

Exhaust Weight: 60g

CDI Weight: 130g

PHIL TEAM PROJECT INCLUDES

2 X DLA180 ENGINE W/ ONE KEY STARTER/GENERATOR GST INC, EACH $4438 USD SUB TOTAL $8876 USD

3 X FALCON 32 X 10W , EACH $156 USD, SUBTOTAL $468 USD

3 X FALCON 32 X 12, EACH $156 USD, SUBTATAL $468 USD

TOTAL $9812 USD GST INC, FREE SHIPPING

*Two strokes;

*Air cooling;

*Electronic closed-loop control;

*Dual redundant speed sensor

*Optional enlightening motor/generator;

*Independent development of engine, ECU and fuel pump;

*Better environmental adaptability;

*Lower specific fuel consumption to meet the needs of long endurance;

*More convenient to use;

*Higher durability reliability;

Model number: B2G70

Displacement: 70ccm

Maximum power: 7HP

Speed range :1800 to 8500rpm

Suitable fuel :92# gasoline

Minimum specific fuel consumption: 435g/kwh

Fuel system: Electronic control

Ignition system: Electronic control

Lubrication mode: mixed lubrication of fuel oil and lubricating oil, lubricating oil/fuel ratio: 1:40 output shaft rotation counterclockwise (from the output shaft end)

Cooling method: Air cooling

Throttle control mode: throttle electronic control

Applicable temperature: -30 Celsius ~+55 Celsius

Starting altitude: 4000 m

Weight composition

Engine body: 2200 g

ECU: 169 g

Fuel pump :213 g

CDI :159 g

Wiring harness :166 g

Exterior dimension

Length x width x height: 173 x 262.5 x 223 mm

Other configurations are optional

Damping system

Inspired integrated configuration/generator configuration

Recommended propeller specification

Two blades :24x10, 24x12, 24x14, 22x12, 22x14

Three-bladed paddle: /

The 498CC engine is an air cooled horizontally opposed piston engine with dual-redundant TCI ignition. Compared with its counterparts in the market,the engine is light weighted, consistent in performance, robust and maintenance friendly. 498CC is an ideal choice to power fixed-wing UAV and VTOL of MTOW 150kg~ 250kg.

Technical Parameter

Engine model: 498CC

Basic structural form: dual -cylinder horizontal confrontation

The engine rotation: counterclockwise (facing the propeller to install flange disk)

Power: 25.5kw@6500rpm

Maximum torque: 40.5N·M@4500rpm

Disted: 498ml

Cycloping: 75mm

Itinerary: 56mm

Compression ratio: 10.6: 1

Maximum speed: 6800rpm

Minimum stable speed: 1800rpm ~ 2200rpm

Working environment temperature: -35 °C ~ 55 °C

Best working temperature: 140 °C ≤ cylinder head temperature ≤ 240 °C

Limited temperature of the cylinder head: 90 °C ≤ cylinder head temperature ≤260 °C,

The running time above 260 °C must not exceed 60s

Fuel: Hybrid fuel (oil: fuel: fuel = 1: 50, volume ratio)

The weight of the whole machine (dry weight): 20.5kg (including ECU, GMU, ignition coil division component, Fuel pump, fuel filter, engine wire beam, fuel pipe Road, sensor, etc.)

Large Repair Spirit (TBO): 300H

The 498CC engine is an air cooled horizontally opposed piston engine with dual-redundant TCI ignition. Compared with its counterparts in the market,the engine is light weighted, consistent in performance, robust and maintenance friendly. 498CC is an ideal choice to power fixed-wing UAV and VTOL of MTOW 150kg~ 250kg.

Technical Parameter

Engine model: 498CC

Basic structural form: dual -cylinder horizontal confrontation

The engine rotation: counterclockwise (facing the propeller to install flange disk)

Power: 25.5kw@6500rpm

Maximum torque: 40.5N·M@4500rpm

Disted: 498ml

Cycloping: 75mm

Itinerary: 56mm

Compression ratio: 10.6: 1

Maximum speed: 6800rpm

Minimum stable speed: 1800rpm ~ 2200rpm

Working environment temperature: -35 °C ~ 55 °C

Best working temperature: 140 °C ≤ cylinder head temperature ≤ 240 °C

Limited temperature of the cylinder head: 90 °C ≤ cylinder head temperature ≤260 °C,

The running time above 260 °C must not exceed 60s

Fuel: Hybrid fuel (oil: fuel: fuel = 1: 50, volume ratio)

The weight of the whole machine (dry weight): 20.5kg (including ECU, GMU, ignition coil division component, Fuel pump, fuel filter, engine wire beam, fuel pipe Road, sensor, etc.)

Large Repair Spirit (TBO): 300H

About this product

Includes generated contents

Precise Engine Testing: The WF-EN-MAX Engine Test Bench is designed for precise testing and analysis of UAV engines, ensuring accurate results and reliable data.

High-Performance Capabilities: With a maximum thrust of 300kgf and supporting up to 50kg of hanging weight, this test bench is suitable for various engine testing needs, including custom requirements.

User-Friendly Interface: The English user interface makes it easy for customers to operate and navigate the device, even for those who may not be fluent in Chinese.

Customization Options: The test bench offers customized support for customers, allowing for tailored solutions to meet specific testing needs, as requested by a user.

Key attributes

Other attributes

customized support OBM

model number WF-EN-MAX

Max Propeller 90inch

Max Thrust 300KGF

English User Interface

Max hanging Weight 50KG support custom

Software MET-Engine Series

LYWF-EN-15 Engine Test Bench

The WF-EN-15 Drone Engine Test Bench is a specialized testing solution designed specifically for the rigorous demands of drone propulsion systems. Tailored for use in research, development, manufacturing, and maintenance environments, this engine test bench integrates advanced measurement technology and automated control systems to ensure precise evaluation of drone engine performance parameters. The WF-EN-15 is an essential tool for optimizing drone flight efficiency and reliability.

Suggested Engine 35cc--110cc Engine

Max Hanging Type Engine 10kg

Max Thrust 50KG

Max Propeller 50 inch

Torque 50 N•m

Optical RPM 0-15000RPM

Pulse RPM 0-60000RPM

Power Supply 12V/24V 2A DC5521

LYWF-EN-17 Engine Test Bench(Contact us for pricing)

LYWF-EN-50 Engine Test Bench

The WF-EN-50 Engine Test Bench is designed to meet the rigorous demands of modern engine and motor testing. Whether you are in the automotive, aerospace, or industrial sectors, this advanced test bench offers the precision, reliability, and flexibility required to evaluate motor performance comprehensively.

Suggested Engine 110cc-350cc Engine

Max weight Engine 20kg

Max Thrust 150KG

Max Propeller 60 inch

Torque 150 N•M

Optical RPM 0-15000RPM

Pulse RPM 0-60000RPM

Power Supply 12V/24V 2A DC5521

LYWF-EN-55 Engine Test Bench

DESCRIPTION:

4-Cylinder

2-Stroke Air Cooled Engine By Opposed Cylinde Electromagnetic Ignition (Charger And Coil)

Diaphragm Carburetor

Electrical Starter 12V (Optional)

Brushless Generator 850W 12V Or 28V (Opional)TBO 100 hrs

Weight kg

Engine Without Propeller 16

POWER

50 hp(With 30*35 Propeller) 6500 RPM

TORQUE

51 Nm 6500 RPM

(With 30*25 Propeller)

MAX RPM

With 30*-25 Propeller 6700 RPM

BoRE STROKE

66mm 40 mm

DISPLACEMENT FUEL

90 Octane (Regular) Gasolines.Mixed With Suitable Two Cycle Oil

OIL

Suitable semi-synthetic 2 stroke motorcycle oil or "Castrol TTS” or “Castrol Power 1" or synthetic oil to the ratio of 25:lor 50:1

MAIN PRODUCT FEATURES

Boxer 2 cylinders,2-stroke

Suitable for heavy fuel: diesel, RP-3/RP-5

Low fuel con sum ption, Io ng-endurance

Compression combustio.stable and reliable power output

Maximum use altitude 5000m

TBOtime>500h

MAIN PRODUCT FEATURES

Boxer 2 cylinders,2-stroke

RP-3/RP-5

Suitable for heavy fuel: diesel, RP-3/RP-5

Low fuel consumption, Io ng-endurance

Compression combustion,stable and reliable power output

Maximum use altitude7000m TBO time>500 Hour

TBOtime>500h

NGH have been known for producing high-quality gasoline engines.NGH is also the first factory in China that independently develops and produces 4-stroke RC gasoline engines.GF38 is a professional-grade 4-stroke gasoline engine built by NGH engineers for model enthusiasts, high performance, low fuel consumption, large torque, low noise, compact structure and beautiful appearance.

GF38 has the installation size of 160-240 glow size 4 stroke engine, and it has power comparable to a 160-240. It is suitable for RC aircraft with takeoff weights of 8-12kg and is the best power configuration for the 160-240 level RC aircraft.

GF38 uses a CM6 spark plug and has standard NGH directional exhaust pipe to make the low voice and high power. The CNC carved and anodized adjustable-length T-type engine mount is equipped to make the engine installation more stable and less vibration.

The rear carburetor facilitates engine adjustment, connecting rod with needle bearing can lubricate the hinge pin better, and unique double piston ring (one lubricating ring and one sealing ring) can seal and lubricate better. The cylinder liner is made of wear-resistant nodular cast iron, the tolerance of the bore in the cylinder is within 0.01mm, and the precision is much higher than the roundness tolerance of the inner hole of the aluminum alloy chrome-plated cylinder liner 0.03mm, aluminum alloy plating chromium cylinder liner in principle does not meet the Eu environmental regulations.

GF38 features:

* NGH directional exhaust muffler for low voice

* The matched Walbro carburetor for reliable running and convenient installation

* CNC carved and adjustable T-shaped engine mount for more stable engine installation and less vibration

* CNC carved double needle roller bearing connecting rod

* Double nut locking output shaft

* RCEXL Ignition with automatic advancing system, especially made for NGH

* RCEXL spark plug CM6

* High-quality bearings

Exhaust size:

GF38-GE( 4-Stroke RC Gasoline Engines with Integrated electric starter and power generation) Technical Parameters

Displacement: 37.97cc

Bore:39mm

Stroke:31.8mm

Practical speed range: 1800-8000rpm

Output power: 3.58HP/8300rpm

Static Thrust: 7.2kg

Fuel: 92# unleaded gasoline + fully synthetic 2T lubricant

Lubrication Ratio: 35:1

Compression Ratio: 9:1

Weight of Engine: 1310g

Weight of Exhaust: 19g

Weight of Ignition: 105g

Ignition Power: DC4.8V-8.4V 1000mAH

Spark plug type: CM-6

Recommended Propeller:18x8-10 19x8-10 20x8

Engine power: 4.22HP/3.58hp

Integrated start-up and power generation:

(1)Control with no induction (no Hall),

(2)starting voltage:Not less 12V starting current: <30A,

(3)Generator output:DC12V,150W/6000rpm

Weight :

(1)electrical machinery>250g,

(2)Weight of control system and voltage stabilizing system>150g

BO 50-100HOURS

This engine is mainly used for fixed-wing with take-off weights (including Gasoline) not more than 12 KGS. Its crankcase, crankshaft, central screws are all made of domestic high-performance materials by CNC processing method. With beautiful appearance, high-precision, drop resistance, fatigue resistance, good stability, strong power performance, we get good reputations from plane enthusiasts after more than 4 years continuously upgrade. Our company will be grateful for your valuable guidance and advice!!

What is the difference in between hobby engine & UAV engine

UAV engine is designed for industrial use and long endurance. The materials used for UAV engine shaft/piston ring etc are all in A grade material in order to achieve the performance.

All the UAV engines with all in one (Generator/autostarter) only for pre-order. Production time nromally takes 20-30 days.

One key start, dc power generation;

Starting input voltage 24V, 28V optional,

power generation output power 400W, 600W optional;

32cc , 58cc , 64cc , 116cc and 180cc, various types of optional;

Accept professional custom, welcome to call or email consultation!

For more quantity order, just click x quantity to select, each pack includes 10 x quanity, i.e, for 50 quantity, select the pack x 5

For the order more than 100 quantity,, contact us for the coupon code.

BULK ORDER NEEDS 40 DAYS. COMBO PACK HAS 10 X SERVOS QUANTITY)

FOR THE ORDER (TOTAL QUANTITY SERVOS ARE 50), JUST ORDER X 5 (EACH PACK HAS 10 SERVOS)

* two cylinders horizontally opposed; (ENGINE TESTED AND APPROVED BY APOLLO-15G VTOL drone to achieve over 20 Hours endurance)

* Two strokes;

* Air cooling;

* Dual redunDant speed sensor;

* electronic closed-loop control;

* Optional One Key Starter/generator;

* Own IP development of engine, ECU and fuel pump; (not select the after market one)

* Better environmental adaptability;

* Lower specific fuel consumption to meet the needs of long endurance;

* Engine thermal management technology to ensure engine stability and long TBOH

* The engine body is always in an appropriate temperature range with integrated cooling mounting ;

* Easier to use;

* Higher durability reliability;

24/7 Technical support by teamaustars for protocol integration and support

Model number :B2H120

Displacement :120ccm

Maximum power :10HP

Speed range :1800 to 8000rpm

Applicable fuel :RP-3

Minimum specific fuel consumption: 390g/kwh

Fuel system: Electronic control

Ignition system: Electronic control

Lubrication mode: mixed lubrication of fuel oil and lubricating oil, lubricating oil/fuel oil ratio: 1:50

Cooling method: Air cooling

Throttle control mode: throttle electronic control

Applicable temperature :-30 Celsius ~+55 Celsius

Starting altitude 4000 meters

Output axis rotation: counterclockwise (from the end of the output axis)

Weight composition

Engine body :3620 g

ECU: 169 g

Fuel pump :213 g

CDI :175 g

Wiring harness :166 g

Exterior dimension

Length x width x height: 243 x 330.2 x 242.3mm

Other configurations are optional

Damping system

Inspired integrated configuration/generator configuration

Recommended propeller specification

Two-bladed paddle: 24x18, 26x14, 26x12, 28x12

Three-bladed paddle: /

UAV VTOL Herlea 265kg Thrust Motor UN233S Combo w/400V/160A ESC & 1X Propeller 78 inch

Motor

Model: UN233S

KV: 13KV

No-load current: 1.5A/30V

Motor weight:14000 g

Maximum current:158A

Maximum tension:265kg

Electrical recommendation:ESC 400V 150A Dual mode

Rated operating voltage:400V

Interphase internal resistance:250mΩ

Leakage current:10mA

Maximum power:62454W

Maximum torque:265Nm

Propeller recommendation:JXF78 two leaf

400V 160A PRO ESC

Support 400V high voltage platform, specially for super heavy load

Man-machine customized.

The third generation semiconducting material is silicon carbide

(SiC) MOS tube, as well as mature new energy vehicle drive architecture design, so that it has the advantages of high power density and high efficiency.

Equipped with 12V/1A BEC output for easy integration.

The mature and reliable sensorless FOC algorithm, combined with many years of market verification, forms a perfect development verification system, and promotes high reliability of products.

Product parameter

Model: FF4009

Power modulation type: FOC

Recommended tension: 80~90kg

Recommended battery: 96~100S LiPo

Rated output power: 30KW

Voltage range: 200V~435V

Continuous output current: 160A

Peak output current: 320A (10S)

Maximum speed: 4800RPM(20 poles)

Ambient temperature: -40~50°C

Waterproof rating: IP67

Cooling method: forced air cooling

BEC: 12V/1A

Fixed propeller function: Supported

Motor temperature detection: PT1000

Weight (excluding wire) : 1.7kg

PWM input level: 3.3V/5V

PWM input pulse width: 200~2000uS

PWM input frequency: 5O~5OOHz

Communication interface: CAN*2 (CAN2.0B, 1M bps)

Digital communication throttle: Supported

Firmware upgrade: Supported

Electrical protection strategy: 1. Locked-rotor protection, overcurrent protection; 2. Short circuit protection, overvoltage protection; 3. Undervoltage protection, input signal identification; 4. Overheat power protection, throttle loss protection

PWM

PWM Pulse Width (uS) Motor speed

Forward Direction 1100 ~ 1900 Idle speed to full throttle speed

Forward Direction 1900 ~ 2400 Full throttle speed

Stop Other Pulse 0 RPM

*Idle speed: The minimum speed, for example, 300RPM, can be set on the firmware.

*Full throttle maximum speed: The maximum speed, such as 5000RPM, can be set on the firmware.

Firmware upgrade

1. Upper computer: Sinemotion Tool

2. Upgrader: USB to CAN;

3. Battery or DC power supply;

Method

1. Connect USB to CAN converter between PC and ESC using CANH, CANL and GND;

2. Power on the power supply.

3. On the Firmware page of the ESC test tool, select the serial port, select the firmware file, and click Update.

78 inch Propeller

UAV VTOL Herlea 200kg Thrust Motor BJO210S Combo w/400V/160A ESC & 1X Propeller 72 inch

Motor

Model: BJO210S

KV: 11KV

Rated power:18KW

Maximum power: 45KW

Number of magnetic steel poles: 42 poles

Rated voltage :400V

Weight: 11kg

400V 160A PRO ESC

Support 400V high voltage platform, specially for super heavy load

Man-machine customized.

The third generation semiconducting material is silicon carbide

(SiC) MOS tube, as well as mature new energy vehicle drive architecture design, so that it has the advantages of high power density and high efficiency.

Equipped with 12V/1A BEC output for easy integration.

The mature and reliable sensorless FOC algorithm, combined with many years of market verification, forms a perfect development verification system, and promotes high reliability of products.

Product parameter

Model: FF4009

Power modulation type: FOC

Recommended tension: 80~90kg

Recommended battery: 96~100S LiPo

Rated output power: 30KW

Voltage range: 200V~435V

Continuous output current: 160A

Peak output current: 320A (10S)

Maximum speed: 4800RPM(20 poles)

Ambient temperature: -40~50°C

Waterproof rating: IP67

Cooling method: forced air cooling

BEC: 12V/1A

Fixed propeller function: Supported

Motor temperature detection: PT1000

Weight (excluding wire) : 1.7kg

PWM input level: 3.3V/5V

PWM input pulse width: 200~2000uS

PWM input frequency: 5O~5OOHz

Communication interface: CAN*2 (CAN2.0B, 1M bps)

Digital communication throttle: Supported

Firmware upgrade: Supported

Electrical protection strategy: 1. Locked-rotor protection, overcurrent protection; 2. Short circuit protection, overvoltage protection; 3. Undervoltage protection, input signal identification; 4. Overheat power protection, throttle loss protection

PWM

PWM Pulse Width (uS) Motor speed

Forward Direction 1100 ~ 1900 Idle speed to full throttle speed

Forward Direction 1900 ~ 2400 Full throttle speed

Stop Other Pulse 0 RPM

*Idle speed: The minimum speed, for example, 300RPM, can be set on the firmware.

*Full throttle maximum speed: The maximum speed, such as 5000RPM, can be set on the firmware.

Firmware upgrade

1. Upper computer: Sinemotion Tool

2. Upgrader: USB to CAN;

3. Battery or DC power supply;

Method

1. Connect USB to CAN converter between PC and ESC using CANH, CANL and GND;

2. Power on the power supply.

3. On the Firmware page of the ESC test tool, select the serial port, select the firmware file, and click Update.

72 inch Propeller

UAV VTOL Herlea 100kg Thrust Motor BJO186D Combo w/400V/50A ESC & 1X Propeller 63 inch

Motor

Model: BJO186D

KV: 12KV

Maximum power: 20KW

Number of magnetic steel poles: 28 poles

Rated voltage :400V

Rated power: 10KW

Weight: 4.6kg

400V 50A ESC

*Support 400V high voltage platform, specially for super heavy load Man-machine customized.

*The use of the third-generation semiconducting material carbonized silicon (SiC) MOS tube, as well as mature new energy vehicle drive architecture design, so that it has the advantages of high power density and high efficiency.

*Equipped with 12V/1A BEC output for easy integration.

*The mature and reliable sensorless FOC algorithm, combined with many years of market verification, forms a perfect development verification system, and promotes high reliability of products.

Product parameter

Model: FF4009

Power modulation type: FOC

Recommended tension: 80~90kg

Recommended battery: 96~100S LiPo

Rated output power: 30KW

Voltage range: 200V~435V

Continuous output current: 160A

Peak output current: 320A (10S)

Maximum speed: 4800RPM(20 poles)

Ambient temperature: -40~50°C

Waterproof rating: IP67

Cooling method: forced air cooling

BEC: 12V/1A

Fixed propeller function: Supported

Motor temperature detection: PT1000

Weight (excluding wire) : 1.7kg

PWM input level: 3.3V/5V

PWM input pulse width: 200~2000uS

PWM input frequency: 5O~5OOHz

Communication interface: CAN*2 (CAN2.0B, 1M bps)

Digital communication throttle: Supported

Firmware upgrade: Supported

Electrical protection strategy: 1. Locked-rotor protection, overcurrent protection; 2. Short circuit protection, overvoltage protection; 3. Undervoltage protection, input signal identification; 4. Overheat power protection, throttle loss protection

PWM

PWM Pulse Width (uS) Motor speed

Forward Direction 1100 ~ 1900 Idle speed to full throttle speed

Forward Direction 1900 ~ 2400 Full throttle speed

Stop Other Pulse 0 RPM

*Idle speed: The minimum speed, for example, 300RPM, can be set on the firmware.

*Full throttle maximum speed: The maximum speed, such as 5000RPM, can be set on the firmware.

Firmware upgrade

1. Upper computer: Sinemotion Tool

2. Upgrader: USB to CAN;

3. Battery or DC power supply;

Method

1. Connect USB to CAN converter between PC and ESC using CANH, CANL and GND;

2. Power on the power supply.

3. On the Firmware page of the ESC test tool, select the serial port, select the firmware file, and click Update.

63 inch Propeller

UAV VTOL Herlea 180kg Thrust Motor BJO186SN-2 Combo w/400V/160A ESC & 1X Propeller 63 inch

Motor

Model:BJO186SN-2

KV: 14KV

Maximum power: 40KW

Number of magnetic steel poles: 28 poles

Rated voltage :400V

Rated power: 13KW

Weight: 9.3kg

400V 160A ESC

Support 400V high voltage platform, specially for super heavy load

Man-machine customized.

The third generation semiconducting material is silicon carbide

(SiC) MOS tube, as well as mature new energy vehicle drive architecture design, so that it has the advantages of high power density and high efficiency.

Equipped with 12V/1A BEC output for easy integration.

The mature and reliable sensorless FOC algorithm, combined with many years of market verification, forms a perfect development verification system, and promotes high reliability of products.

Product parameter

Model: BJO - 400 -110AX2

Power modulation type: FOC

Recommended tension: 80~90kg

Recommended battery: 96~100S LiPo

Rated output power: 30KW

Voltage range: 200V~435V

Continuous output current: 160A

Peak output current: 320A (10S)

Maximum speed: 4800RPM(20 poles)

Ambient temperature: -40~50°C

Waterproof rating: IP67

Cooling method: forced air cooling

BEC: 12V/1A

Fixed propeller function: Supported

Motor temperature detection: PT1000

Weight (excluding wire) : 1.7kg

PWM input level: 3.3V/5V

PWM input pulse width: 200~2000uS

PWM input frequency: 5O~5OOHz

Communication interface: CAN*2 (CAN2.0B, 1M bps)

Digital communication throttle: Supported

Firmware upgrade: Supported

Electrical protection strategy: 1. Locked-rotor protection, overcurrent protection; 2. Short circuit protection, overvoltage protection; 3. Undervoltage protection, input signal identification; 4. Overheat power protection, throttle loss protection

PWM

PWM Pulse Width (uS) Motor speed

Forward Direction 1100 ~ 1900 Idle speed to full throttle speed

Forward Direction 1900 ~ 2400 Full throttle speed

Stop Other Pulse 0 RPM

*Idle speed: The minimum speed, for example, 300RPM, can be set on the firmware.

*Full throttle maximum speed: The maximum speed, such as 5000RPM, can be set on the firmware.

Firmware upgrade

1. Upper computer: Sinemotion Tool

2. Upgrader: USB to CAN;

3. Battery or DC power supply;

Method

1. Connect USB to CAN converter between PC and ESC using CANH, CANL and GND;

2. Power on the power supply.

3. On the Firmware page of the ESC test tool, select the serial port, select the firmware file, and click Update.

63 inch Propeller

Size: 63 inches carbon fiber light steel wood

Weight of single paddle: 1 kg

UAV VTOL Herlea 150kg Thrust Motor TY227D Combo w/400V/80A ESC & 1X Propeller 63 inch

Motor

Model: TY227D

KV: 13 KV

Rated power: 13 KW

Maximum power: 35 KW

Rated voltage: 400 V

Weight: 7.98kg

Number of magnetic steel poles: 42 poles

Voltage range: 300-420V

Rated tension: 75kg

Maximum tension :154.5kg

Voltage :360V

400V 80A ESC

*Support 400V high voltage platform, specially for super heavy load Man-machine customized.

*The use of the third-generation semiconducting material carbonized silicon (SiC) MOS tube, as well as mature new energy vehicle drive architecture design, so that it has the advantages of high power density and high efficiency.

*Equipped with 12V/1A BEC output for easy integration.

*The mature and reliable sensorless FOC algorithm, combined with many years of market verification, forms a perfect development verification system, and promotes high reliability of products.

Product parameter

Model: FF4009

Power modulation type: FOC

Recommended tension: 80~90kg

Recommended battery: 96~100S LiPo

Rated output power: 16KW

Voltage range: 200V~435V

Continuous output current: 80A

Peak output current: 150A (10S)

Maximum speed: 4800RPM(20 poles)

Ambient temperature: -40~50°C

Waterproof rating: IP67

Cooling method: forced air cooling

BEC: 12V/1A

Fixed propeller function: Supported

Motor temperature detection: PT1000

Weight (excluding wire) : 1.5kg

PWM input level: 3.3V/5V

PWM input pulse width: 200~2000uS

PWM input frequency: 5O~5OOHz

Communication interface: CAN*2 (CAN2.0B, 1M bps)

Digital communication throttle: Supported

Firmware upgrade: Supported

Electrical protection strategy: 1. Locked-rotor protection, overcurrent protection; 2. Short circuit protection, overvoltage protection; 3. Undervoltage protection, input signal identification; 4. Overheat power protection, throttle loss protection

PWM

PWM Pulse Width (uS) Motor speed

Forward Direction 1100 ~ 1900 Idle speed to full throttle speed

Forward Direction 1900 ~ 2400 Full throttle speed

Stop Other Pulse 0 RPM

*Idle speed: The minimum speed, for example, 300RPM, can be set on the firmware.

*Full throttle maximum speed: The maximum speed, such as 5000RPM, can be set on the firmware.

Firmware upgrade

1. Upper computer: Sinemotion Tool

2. Upgrader: USB to CAN;

3. Battery or DC power supply;

Method

1. Connect USB to CAN converter between PC and ESC using CANH, CANL and GND;

2. Power on the power supply.

3. On the Firmware page of the ESC test tool, select the serial port, select the firmware file, and click Update.

63 inch Propeller

TEAM AUSTARS PROVIDE ONLINE 24/7 TECHNICAL SUPPORT AND CUSTOMER SERVICE, TRAINING

THE PACKAGE INCLUDES THE COMPLETE PRODUCT AND TECHNICAL SUPPORT 24/7 ONLINE BY TEAMAUSTARS

DLE170M EFI One Key Starter/Generator Version (14V/350W Generator)

DLE170 is an upgraded product of the previous RC Model engine DLE170 version. We have redesigned the entire structure

of the enginein order to providea better power. The new planetary gear starting mechanism has replaced the complex starting system in

earlier versions.It's not only simplifies the number of parts be used, also reduces the weight of the engine and the failure rate. The new version of

engine now is capable for multi-task purposes. We can now provide different rotation (counter-clockwise , clockwise) and in-build generator kit.

Planetary gear starter assembly

It has small size with high torque, high durability, more reliable choice for paramotor, UAV and other projects.

The output gear will only extend and drive the engine while starting the engine. After the engine is started and the starter stopped,the output gear will disengage and retract to back.

170 Generator version

170 Integrated Starter(EFI One Key Starter)

weight

Engine+Muffler 5900g

Lgniter+Spark plug 265g

Relay 160g

Rectifier 415g

Engine+Muffler 5900g

Lgniter+Spark plug 265g

Relay 160g

Parameter

performance 17.5HP/7500rpm

Diameter × Stroke 52mm × 40mm

Recommended Propeller 32x10 32x12

Compression Ratio 9.5 : 1

Lubrication Ratio 30 : 1

Displacement 170cm³

Spark Plug Type NGK CMR7H

Starting motor power 12V 400W

Generator voltage 14.5V

Generator power 350W/6000rpm

performance 17.5HP/7500rpm

Diameter × Stroke 52mm × 40mm

Recommended Propeller 32x10 32x12

Compression Ratio 9.5 : 1

Lubrication Ratio 30 : 1

Displacement 170cm³

Spark Plug Type NGK CMR7H

Starting motor power 12V 400W

FOR INTEGRATION WITH ENGINE PROTOCOL, CONTACT TEAM AUSTARS FOR 24/7 TECHNICAL SUPPORT

ONE OF THE BEST VALUE EFI 170CC ENGINE FOR UAV MARKET, SAVE FUEL SAVE COST. APPROVED BY THE MARKET

STANDARD PACKAGE:

ENGINE, FUEL PUMP, FUEL FILTER, ECU HARNESS, IGNITION, MOUNTING SYSTEM, EXHAUST PIPES

PRODUCT WARRANTY: TBO 300HOURS OR ONE YEAR. THE ONE COMING FIRST APPLIED. SUPPORTING ECU/232/422, CAN, PWM COM & CONTROL, PROTOCOL FOR SYSTEM INTEGRATION BE SUPPLIED

Horizontally opposed, two cylinders;

* two cylinders horizontally opposed;

* Two strokes;

* Air cooling;

* Dual redundant speed sensor;

* electronic closed-loop control;

* Optional enlightening motor/generator

* Hone de power independent development;

* Better environmental adaptability;

* Lower specific fuel consumption to meet the needs of long endurance;

* Easier to use;

* Higher durability reliability;

Model number :B2G170

Displacement :170ccm

Maximum power :15HP

The rotational speed ranges from 1800 to 7800rpm

Suitable fuel :92# gasoline

Minimum specific fuel consumption: 412g/kwh

Fuel system: Electronic control

Ignition system: Electronic control

Lubrication mode: mixed lubrication of fuel oil and lubricating oil, lubricating oil/fuel oil ratio: 1:40

Cooling method: Air cooling

Throttle control mode: throttle electronic control

Applicable temperature :-30 Celsius ~+55 Celsius

Starting altitude 4000 meters

Output axis rotation: counterclockwise (from the end of the output axis)

Weight composition

Engine body :4153 g

ECU: 169 g

Fuel pump :213 g

CDI :175 g

Wiring harness :166 g

Exterior dimension

Length x width x height: 259 x 288.4 x 202.4 mm

Other configurations are optional

Damping system

Inspired integrated configuration/generator configuration

Recommended propeller specification

Two blades: 26x18, 28x16, 28x14, 30x12, 30x10

Three-blade paddle: 24x18, 24x16, 25x12, 25x14

* two cylinders horizontally opposed; (engine was approved & integrated with many branded VTOLs worldwide)

* Two strokes;

* Air cooling;

* electronic closed-loop control;

* Dual redundant speed sensors

* Optional enlightening motor/generator

* Independent development of engine, ECU and fuel pump;

* Better environmental adaptability;

* Lower specific fuel consumption to meet the needs of long endurance;

* Engine thermal management technology to ensure engine

* The body is always in an appropriate temperature range;

* Easier to use;

* Higher durability reliability;

24/7 Technical support by teamaustars for protocol integration and support

Model number :B2H70

Displacement :70ccm

Maximum power :6HP

Speed range :1800 to 8500rpm

Applicable fuel :RP-3

Minimum specific fuel consumption: 405g/kwh

Fuel system: Electronic control

Ignition system: Electronic control

Lubrication mode: mixed lubrication of fuel oil and lubricating oil, lubricating oil/fuel oil ratio: 1:50

Cooling method: Air cooling

Throttle control mode: throttle electronic control

Applicable temperature :-30 Celsius ~+55 Celsius

Starting altitude 4000 meters

Output axis rotation: counterclockwise (from the end of the output axis)

Weight composition

Engine body :2600 g

ECU: 169 g

Fuel pump :213 g

CDI :159 g

Wiring harness :166 g

Exterior dimension

Length x width x height: 195.4 x 262.5 x 270.5mm

Other configurations are optional

Damping system

Inspired integrated configuration/generator configuration

Recommended propeller specification

Two blades: 24x10, 24x12, 24x14, 22x12, 22x14

Three-bladed paddle: /

FOR INTEGRATION WITH ENGINE PROTOCOL, CONTACT TEAM AUSTARS FOR 24/7 TECHNICAL SUPPORT

ONE OF THE BEST VALUE EFI 120CC ENGINE FOR UAV MARKET, SAVE FUEL SAVE COST. APPROVED BY THE MARKET

STANDARD PACKAGE:

ENGINE, FUEL PUMP, FUEL FILTER, ECU HARNESS, IGNITION, MOUNTING SYSTEM, EXHAUST PIPES

PRODUCT WARRANTY: TBO 300HOURS OR ONE YEAR. THE ONE COMING FIRST APPLIED. SUPPORTING ECU/232/422, CAN, PWM COM & CONTROL, PROTOCOL FOR SYSTEM INTEGRATION BE SUPPLIED

Horizontally opposed, two cylinders;

* Two strokes;

* Air cooling;

* Dual redundant speed sensors

* electronic closed-loop control;

* Optional one key starter/generator;

* Own IP development of engine, ECU and fuel pump; (not like other brands with after market ECU)

* Reliable environmental adaptability;

* Lower specific fuel consumption to meet the needs of long endurance;

* Easier to use;

* Higher durability reliability;

Model number :B2G120

Displacement :120ccm

Maximum power :11HP

Speed range :1800 to 8000rpm

Suitable fuel :92# gasoline

Minimum specific fuel consumption: 425g/kwh

Fuel system: Electronic control

Ignition system: Electronic control

Lubrication mode: mixed lubrication of fuel oil and lubricating oil, lubricating oil/fuel oil ratio: 1:40

Cooling method: Air cooling

Throttle control mode: throttle electronic control

Applicable temperature :-30 Celsius ~+55 Celsius

Starting altitude 4000 meters

Output axis rotation: counterclockwise (from the end of the output axis)

Weight composition

Engine body: 3215g

ECU: 169 g

Fuel pump :213 g

CDI :159 g

Wiring harness :166 g

Exterior dimension

Length x width x height: 243 x 263.6 x 192.8 mm

Other configurations are optional

Damping system

Inspired integrated configuration/generator configuration

Recommended propeller specification

Two-bladed paddle: 24x18, 26x14, 26x12, 28x12

Three-bladed paddle: /

Regarding Roto Motor 85cc FS UAV engine (Production & Testing around 20 days)

• There are up to 18 configurations for different solutions.
• The engine has carby version and EFI (Electronic Fuel Injection)
• There are two generator in 400W and 1000W and Voltage regulator in two voltage outputs

Rotomotor makes one key starter (STG/Starter) and EPU (Electric Power Unit)/generator in 1000W and 2000W

STG-EPU (Start Generator-Electric Power Unit)

Rotomotor makes E-Control which Is designed to remote starter, turbo mode, charge and use battery from 12S Lipo battery for the project (servo, RX, camera Gimbal, task payload etc). This is the best solution to integrate other gears (One Key starter/EPU) for long endurance and battery life time circle. It is very useful for both carby version and EFi version

E-Control is an electronic system designed to control the motor generator, which allows the start of the internal combustion engine, charging batteries and hybrid operation, increasing the power of the internal combustion engine

2.1 Absolute Maximum Ratings

Operating temperature: -20°C to +80°C

Non-operational voltage: 9 - 60V DC

Charging current: 45A

Peak power (10 sec): 4300W

Peak current (10 sec): 100A

Safe voltage: 11 - 55V DC

Operating voltage: 12 - 51V DC

Battery configuration: 12 S

Battery nominal voltage: 43.2V DC

PWM frequency: 20 kHz

Controller thermally connected to infinite heat sink which does not exceed 60°C.

Maximal power dissipation: 20W

Nominal power (60 min): 2200W

Nominal current (60 min): 51A

Controller placed in still air of temperature 25°C.

Maximal power dissipation : 10W

Nominal power (60 min): 1500W

Nominal current (60 min): 35A

BMS (Battery Management System) is used for battery lifetime maintenance, which use Lipo, Li-ion, LifePO4 cells or other cells with operation voltage range 1.8V-5V each cell. BMS provides protection and increase the lifetime of the batteries by measuring its temperature, controlling the voltage and flowed current.

Configuration explanation:

If the customer wants to achieve up to 5000 meter altitude and long endurance and long life time of the battery, select Config 85E or F

• Config 85A Carby version engine only,
• Config 85A1 EFI (Electronic Fuel Injection) version engine only.
• Config 85B Carby engine+Generator 400W+Regulator w/two outputs
• Config 85B1 EFI engine+Generator 400W+Regulator w/two outputs
• Config 85C Carby engine+Generator 1000W+Regulator w/two outputs
• Config 85C1 EFI engine+Generator 1000W+Regulator w/two outputs
• Config 85D Carby engine+Starter/EPU (ONE KEY STARTER /POWER GENERATOR) 1000W
• Config 85D1 EFI engine+Starter/EPU (ONE KEY STARTER /POWER GENERATOR) 1000W
• Config 85DA Carby engine+Starter/EPU (ONE KEY STARTER /POWER GENERATOR) 2000W
• Config 85DA1 EFI engine+Starter/EPU (ONE KEY STARTER /POWER GENERATOR) 2000W
• 
  
• Config 85E Carby engine+E-Control Starter/EPU (ONE KEY STARTER /POWER GENERATOR 1000w)+Lipo battery up to 12s (Owner prepares themselves)+BMS-this is the best solution. The user can achive "remote start, turbo mode, chargingand using power from 12S Lipo battery for the project (servos, RX, camera, gimbal, task payload etc)
• Config 85E1 EFI engine+E-Control Starter/EPU (ONE KEY STARTER /POWER GENERATOR)+Lipo battery up to 12s (Owner prepares themselves)+BMS-this is the best option.
• 
  
• Config 85EA Carby engine+E-Control Starter/EPU (ONE KEY STARTER /POWER GENERATOR 2000w)+Lipo battery up to 12s (Owner prepares themselves)+BMS-this is the best solution. The user can achive "remote start, turbo mode, chargingand using power from 12S Lipo battery for the project (servos, RX, camera, gimbal, task payload etc)
• Config 85EA1 EFI engine+E-Control Starter/EPU (ONE KEY STARTER /POWER GENERATOR 2000w)+Lipo battery up to 12s (Owner prepares themselves)+BMS-this is the best solution. The user can achive "remote start, turbo mode, chargingand using power from 12S Lipo battery for the project (servos, RX, camera, gimbal, task payload etc)
• 
  
• Config 85F Carby engine+E-Control Starter/EPU (ONE KEY STARTER /POWER GENERATOR 1000W)+Lipo battery up to 12s (Owner prepares themselves) w/o BMS
• Config85F1 EFI engine+E-Control Starter/EPU (ONE KEY STARTER /POWER GENERATOR 1000W)+Lipo battery up to 12s (Owner prepares themselves) w/o BMS
• Config 85FA Carby engine+E-Control Starter/EPU (ONE KEY STARTER /POWER GENERATOR 2000W)+Lipo battery up to 12s (Owner prepares themselves) w/o BMS
• Config85FA1 EFI engine+E-Control Starter/EPU (ONE KEY STARTER /POWER GENERATOR 2000W)+Lipo battery up to 12s (Owner prepares themselves) w/o BMS

For 85cc EFI version, Engine Management (EngManager) package with control Module/Panel is optional and supplied, which is designed to manage and control petrol engine from one central injector to four sequential injectors, which the flight control display, input voltage, engine temperature,RPM, timer, fuel level info, Fuel flow info, Altitude correction, injection delay, automatic choke/temperture choke at cold engine start, fue tank volume, fuel indicator calibration/cosumption, fuel pump etc can be adjusted.

The engine management package does not need to be connected to a PC, which is often difficult when running the engine on site. It is optional. This package is not necessary unless the customer wants precision settings.

EngManager includes Main unit, injector, fuel pump, fuel filter, 2pcs CHT sensors, main cable connector, Oxygen sensor, controler for oxygen sensor, Glavanic separation module for ignition, control module, and flight control display.

ROTO 85 FS AL is suitable for UAV projects within the range of 4 meters and weight up to 35 kg.

Four-stroke two-cylinder petrol internal combustion engine

	Alternator 400W	Alternator 1000W
PMG ( Permanent Magnet Generator)	3 phase output
NdFeB magnets
Voltage curve	14V/1000RPM (possibility of rewinding according to client)
Diameter	101mm
Thickness	22mm	25mm
Weight	450g	550g
Out. Power at 3000RPM	300W	430W
Out. Power at 6000RPM	600W	960W
Cooling	forced by air flow
Resistance	to fuel, oil, water, mechanical stress
Operating temperature	-30°C to 120°C