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Makeflyeasy Fighter VTOL Specifications
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:
1、”Power System" means only power parts, not the aircraft fuselage
2、If you are failed to place order directly from our web shop, pls contact our sales team to get support.
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
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
Embedded carbon tubes on thevertical tail rudder surface in-crease the strength of rudder sur-face, increase the rudder anglefixing plate, and increase therudder surface response speed Three hinges connect the ruddersurface, reduce the rotation resis-tance and increase the accuracyof rudder surface execution
The left and right horizontaltails are designed with inde-pendent control of dual servo.Even if one side fails, the air-craft can return, which im-proves the safety of the air-craft
Horizontal tail servos do notneed to be buried in advance,which is convenient for servomaintenance The rocker arm of servo adoptsan embedded design, even if therocker arm transmission columnis loose, the rudder surface isalso accurately executed
Carbon tubes are embeddedin the rudder surface of thehorizontal tail to increase thestrength of the rudder surface Four hinges connect therudder surface, reduce the ro.tation resistance and increasethe accuracy of rudder surfaceexecution
ф12x1000mm Outer coveringф14x560mm Main carbon tubeф12x600mm Auxiliary carbon tubeEnsure the overall rigidityof the wing.
The wing and fuselage withthe embedded box structureenhance the contortion resis.tance of the wing
Dual connector can realize signalline redundancy, improve systemstability, reduce wiring difficulty,and is compatible with 4 + 2layout
The wing wiring cabin facili-tates the installation ofpower signal cables. With thewiring board, the wing powersystem can be quickly disas-sembled and assembled
The aileron servo cabin not onlyfacilitates replacing servo, butalso can be equipped with an air-speed meter module to improvethe airspeed detection accuracy
The multi-axis arm can be in-stalled and removed as awhole, which is convenientfor use and maintenance
Embedded carbon tubes onthe Aileron rudder surface in-crease the strength of ruddersurface, increase the rudderangle fixing plate, and in-crease the rudder surface re-sponse speed Four hinges connect therudder surface, reduce therotation resistance and in-crease the accuracy of ruddersurface execution
The fuselage adopts 25mm carbonfiber square tube, which not onlyensures the rigidity but also hasenough space for wiring and casing
The arm adopts self-lockingfolding structure, which canbe folded with one pressand locked with one turn
The multi-axis motor base ismade of aluminum alloy CNC ma-chined, and the surface is anodicoxidized to increase abrasion re.sistance and corrosion resistance
The motor frame supportsthe largest ф60mm motor,and the size of the ESC cabinis 63 x 43 x 13mm with cus-tomize ESC, waterproof anddustproof, good heat dissipa-tion effect, no fear of harshexternal work environment
