Makeflyeasy Fighter VTOL – 1.5KG Payload 150KM Range 2430mm Wingspan MFE Fighter VTOL Compound Wing EPO VTOL Aerial Survey Fix-wing AirCraft Drone RC AirplaneKIT KIT Version

Description

Material: EPO,EVA,carbon fiber,PC,engineering plastics and etc.

Wing Span:2430mm
Fuselage height: 180mm
Fuselage length:1450mm
Suggested fight speed:19-20m/s
Maximum payload: 1.5Kg
Longest flight range: >150km(600g load)
Practical ceiling height: 4000m
Take-off and landing approach: VTOL
Wing area:72.5dm2
Stalling speed: 10m/s
Payload cabin size:280*160*110mm
Max take-off weight:11.5kg
Wind resistance: 5
Dismounting way: tool-free
Transport case seize:1.25mx0.34mx0.49m

Range 1:120min/137km(speed 19m/s load 600g,battery 2pcs 6s 16000mah in series,take-off weight 10KG,altitude 500m)
Range 2:134min/155km(speed 19m/s,load 600g,battery 2pcs 6S 22000mah in series,take-off weight 11.2KG,altitude 500m)

NOTE:

1Power System” means only power parts, not the aircraft fuselage

2If you are failed to place order directly from our web shop, pls contact our sales team to get support.

Download:User manual

two years and iterated 5 versions by the MFE Team
Fighter is a 10kg level VTOL fixed-wing carrier aircraft whitch was optimized repeatedly for

On the basis of the conventional inverted T layout, the Fighter have optimized the aerodynamic figure and relative positions of the wings, horizontal tail, vertical tail, and fuselage

The fuselage adopts the overall streamline figure, and the flight resistance is reduced asmuch as possible while ensuring a large space

BOM/WIRING

WIRING

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BOM

The inside of the fuselage isequipped with a wire groove anda removable baffle, which ismatched with nylon braidedsleeves to ensure simple and ef-ficient wiring in the cabin

Streamlined EVA cushions aredesigned on both sides of thebottom of the fuselage, whichdoes not block the camerahole, shock absorption andwear resistance, and improvethe aircraft’s course stability

The center of gravity of the air-craft is under the raised positionof fuselage hook and the wingroot plastic (same position)

The center of gravity of thehand-held lanyard duringheavy load, and the center ofgravity of the hand-liftedwing during light load

Battery cabin supports 26S@16000/22000mAh(Li-Po)whitch provides strong powerfor long endurance

The battery fixed seat ismade of PC board and CNCmachined, with light weightand good impact resistance
The dual battery cable tiehas a reasonable layout,which effectively avoidsentanglement

cabin supports a maximum installation size of 80 x 45 x 68mm, With large-size and large-pitchpropellers, the front-pull power conversion efficiency is high

The distribution cabin cover isreserved with data transmissionantenna holes, which is conve-nient for the assembly and dis-assembly of the antenna

The design of the distribu-tion cabin shortens the wirepath and improves the elec-tromagnetic environment ofthe aircraft
With the power distributionboard, the power system ofthe fuselage can be quicklyreplaced

Load cabin size:280x160x110mm

A7R/A7R2,five-lenshalf-frame tilt camera canbe placed in the maincabin

The auxiliary carbon tube adoptsa toolless quick-release design.After disassembly, it can openthe main and auxiliary cabin. ltcan be equipped with a five-lensfull-frame tilt camera or a 1.5kglightweight lidar

The open platform design of theflight control cabin facilitates theinstallation of open source /com-mercial flight control installation
Cooperating with the centerboard can make full use of thespace layout, greatly optimizingthe line sequence and direction

The double-sided roundholes ensure the accurateheight measurement of thefight control barometer andalso facilitate the installationand use of safety switches

Cooperate with the flight controlprotective cover to prevent for-eign matter from falling, beautifuland dustproof

The RTK / PPK antenna position isreserved at the rear of the flightcontrol cabin, and with the RTK/PPK module, it can improve thePOS data accuracy

The GPS module is locatedat the rear of the fuselage,with a size of 69 x 63 x18mm, which can accommo.date flight control GPS andcompass modules. The elec-tromagnetic environment isclean

The vertical tail and fuselageadopt a 5-point integrated tool-less quick-release structure

When closed, the plasticparts on both sides form anembedded box structure,which has strong resistanceto compression, tension andtorsion

The 9-pin gold-plated connectoris used to realize the mechani-cal and electrical separation ofthe tail and the fuselage

The vertical tail servo can bedisassembled and assem-bled, which is convenient formaintenance.

The horizontal tail adopts atool-less quick-release structure,which is automatically lockedwhen it is pushed and pulled outimmediately when pressed