Material: EPO, EVA, carbon fibre,engineering plastics, etc.
Wingspan:2430mm
Fuselage height:180mm
Fuselage length:1450mm
Wind Resistance:Class 5
Wing Area:72.5dm²
Max payload:>1.5kg
Take-off and landing mode:parachute/skidding
Disassembly:Tool-less DisassemblyLoad compartment
Stall speed:10m/s(test condition:500m above sea level,10.5kgtake-off weight)
Max speed:25m/s(if over 25m/s, need to strengthen the rudder toavoid losing rudder effect)
Max range:>250km(Test condition:Li-Po6S44000mah,0.6kg load)
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.
Download:User manual
On the basis of the conventional inverted T layout, the Fighter have optimized the aero.dynamic figure and relative positions of the wings, horizontal tail, vertical tail, and fuse-lage
The fuselage adopts the overall streamline fgure, and the fight resistance is reduced asmuch as possible while ensuring a large space
The size of the fuselage at the rear of the fuselage and the distance between the two handsto support the aircraft to achieve the best ergonomic size range, to achieve accurate forceand smooth throw
BOM/WIRING
WIRING
Click EnlargeBOM
Click EnlargeA large number of high-strengthlight PC boards are used in mate-rials, and a large number of em-bedded box structures are usedin figure to improve the structur-al strength and rigidity of thebody in many ways
Based on the "Overload Test"according to the structure andload characteristics of thewing, tail and fuselage, thestructure was optimized as"g" precision to minimize un-necessary weight
The wing and tail adopt a toolless quick-release structure, which reduces the installationsteps and shortens the disassembly and assembly time
The head cabin cover adoptsan integral umbrella structureto prevent rainwater from en-tering the cabin
The fuselage cabin cover isspecially designed with awater channel and a wateroutlet to ensure that the air-craft has normal flight capa-bilities in little rain
The inside of the fuselage isequipped with a wire groove anda removable baffle, which ismatched with nylon braidedsleeves to ensure simple and effi-cient wiring in the cabin
Streamlined EVA cushionsare designed on both sidesof the bottom of the fuse-lage, which does not blockthe camera hole, shock ab-sorption and wear resis-tance, and improve the air-craft'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 centerof gravity of the hand-liftedwing during light load
Battery cabin supports 26s@16000/22000mAh(Li-Po)whitch provides strong power forlong endurance
The battery fixed seat ismade of PC board and CNCmachined, with light weightand good impact resistance
The dual battery cable tie hasa reasonable layout, whicheffectively avoids entangle-ment
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 distributioncabin shortens the wire pathand improves the electromag.netic environment of the air-craft
With the power distributionboard, the power system ofthe fuselage can be quickly re.placed
Load cabin size:280x160x110mm
A7R/A7R2,five-lenshalf-frame tilt camera canbe placed in the main cabin
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 center boardcan make full use of the spacelayout, greatly optimizing the linesequence and direction
The double-sided roundholes ensure the accurateheight measurement of theflight control barometer andalso facilitate the installationand use of safety switches
Cooperate with the flight con-trol protective cover to pre-vent foreign matter from fall-ing, beautiful and dustproof
The RTK/PPK antenna positionis reserved at the rear of theflight control cabin, and with theRTK/PPK module,it can im-prove the POS data accuracy
The GPS module is located atthe rear of the fuselage, witha size of 69 x 63 x 18mm,which can accommodateflight control GPS and com-pass modules. The electro-magnetic environment isclean
The size of the parachute cabin is172 x 113 x52mm, which caneasily place 6-8kg parachute
The horizontal tail adopts atool-less quick-release structurewhich is automatically lockedwhen it is pushed and pulled outimmediately when pressed
The left and right horizontaltails are designed with inde.pendent control of dualservo. Even if one side fails,the aircraft can return,which improves the safetyof the aircraft
Horizontal tail servos do notneed to be buried in advance,which is convenient for servomaintenance
The rocker arm of servoadopts an embedded design,even if the rocker arm transmission column is loose, therudder surface is also accu-rately executed
Carbon tubes are embeddedin the rudder surface of thehorizontal tail to increasethe strength of the ruddersurface
Four hinges connect therudder surface, reduce therotation resistance and in-crease the accuracy ofrudder surface execution
ф12x1000mm Outer coveringф14x560mm Main carbon tubeф12x600mm Auxiliary carbon tubeEnsure the overall rigidity ofthe wing.
The wing and fuselage withthe embedded box struc-ture enhance the contor-tion resistance of the wing
Dual connector can realizesignal line redundancy,im-prove system stability, reducewiring difficulty, and is com-patible with 4 + 2 layout
The wing wiring cabin facil-itates the installation ofpower signal cables. Withthe wiring board, the wingpower system can bequickly disassembled andassembled
The aileron servo cabin notonly facilitates replacingservo, but also can beequipped with an airspeedmeter module to improve theairspeed detection accuracy
Embedded carbon tubes onthe Aileron rudder surfaceincrease the strength ofrudder surface,increase therudder angle fixing plate, andincrease the rudder surfaceresponse speed
Four hinges connect therudder surface, reduce therotation resistance and in-crease the accuracy of
Double forward-pull motor,embedded reinforced boardconnects the wing carbon tubeand the motor frame to ensurethe strength and rigidity of themotor frame
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