Makeflyeasy Striver mini 4+1/4+2 2100mm VTOL UAV

large amounts of high-strength lightweight carbon fiber,woodboard,and PC board are used in materials.

In terms of shape, a largenumber of embedded boxstructures are used to com-prehensively improve thestructural strength and rigidi-ty of the body.

On the basis of "overload ex-periment", according to thestructure and loading charac-teristics of the wing, tail, andfuselage.Optimize the structure ac-cordingto the g precision tominimize unnecessarweight.

Striver mini VTOL supports 4+1 mode and 4+2 mode.

The wing and tail adopt tool-less quick disassembly structure to reduce the installation stepsand shorten the disassembly and assembly time.

The inner liner of the packing box is made of high-magnification EPS foam.Light specific gravity, impact resistance, good shockproof effect, suitable for long-distancetransportation.

The bottom of the fuselageadopts a three-point type supportmechanism, ground clearancehigh, not covering the camerhole,improveaircraft heading stability.

The center of gravity of theaircraft is in the fuselageunder the center hook andwing root plastic projection(same location)
When the load is heavy, thelanyard is used to carry thecenter of gravity; when theload is light, the center ofgravity of the wing is lifted byhand.

The inside of the fuselage isde-signed with a wire slot and a removable baffle.It is convenient for the installa-tion of the wires, and at thesame time ensures the conciseand efficient wiring in the cabin.

The motor base of the machinehead is made of PC alloy plastic,which has strong impact resis-tance, and can support the outerrotor ф60mm motor at most.

The ESC cover adopts a hollowgrid design, which is light inweight and good in heat dissi-pation.

The ESC adopts a built-indesign,and the maximum supportedsize is 71x38mm.

The size of the battery compart-ment is 260x130x72mm,and thelargest support 6S@30000mahbattery,to provide the possibilityof a longer range.
The battery holder is made of PCboard CNC processing, which islight in weight and has goodimpact resistance.

The battery ties have a reasona-ble layout, which is convenientfor binding and unbinding, andeffectively avoids entanglement.

The power distribution compart-ment is made ofinjection moldedengineering plastic,improve thestructural strength of the fuselage.

(Optional) 2-channel redundantflight control power supply inte-grated in the power distributionboard, 1 way servo powersupply, 1 way load power supplyshortened wire path, reducedsoldering process, clean and tidywiring.

The hatch is reserved for the digitaltransmission antenna hole, whichis convenient to install and removethe antenna.

Load compartment size.220x150x110mm. Can hold Sony A7Rseries cameras and five-lens tiltcamera.

The auxiliary carbon tube adoptsa tool-ess quickrelease design,which is convenient for carryinglarger loads.
Reserved for common lens cut-ting holes, easy to open thehole.

The flight control cabin adopts aplatform-based open design,compatible with open source/commercial flight controlinstallation.
(Optional) The center panel canmake full use of the spacelayout, extremely Optimize theorder and direction of the wires.

The GPS cabin is located at therear of the fuselage, the size of78x58x37 mm can place theGPS and compass module, andthe electromagnetic environ-ment is clean.

The position of the PPKantenna is reservedbehind the GPS cabin,it isconvenient to install PPKantenna to improve theaccuracy of POS data.

The wing adopts ф12x900mmmain carbon tube and ф10x530mmsecondary carbon tube. Ensure theoverall rigidity of the wing,

The wing and fuselage arecustomized industrial-grade9+2 high-current connectorsrealize the synchronousseparation of electrical andstructure.

Pre-embedded carbon tubes onthe aileron increase the strengthof the aileron.Increase the servo angle fixingplate,and improve the responsespeed.
The hinge connects the aileronto increase the accuracy anddurability of the aileron execu-tion.

The multi-rotor part of thewing is reinforced with 3Mstickers, which increases therigidity of the aircraft and im-proves the torsion resistanceof the wing.

The rotor arm can be installedand removed as a whole, which iseasy to use and transport.
The mid-end of the arm adopts a20mm carbon fiber square tube,which fits closely with the mainand auxiliary carbon tubes of thewing to ensure rigidity.

The square tube and the roundtube adopt the aluminum alloyself-locking folding structure,which can be folded by onepress and self-locked by oneturn, which is easy to use.

The multi-rotor motor base isprocessed by aluminum alloy CNC.The surface adopts anodizingprocess to increase wear resis-tance and corrosion resistance.

The motor base supports thelargest outer rotor ф65 mmmotor, the size of the ESCcabin is 67x31x12mm.(Optional) Customized Esc,waterproof and dustproof,good heat dissipation effect,no fear of harsh field enviro-nment.

The wing motor base adopts anembedded box structure toconnect with the main carbontube of the wing, which is stableand reliable.The motor base supports themaximum outer rotor diameterф44mm motor (used in 4+2 mode).

Dimensions of the wing ESCcabin:80x33x25mm,easy toinstall ESC, ESC cover adoptshollow grid design, light weightand good heat dissipation.

Adaptor cabin is designed in themiddle of the wing to facilitatethe installation of ESC and servowires.
(Optional) Wiring board for quickdisassembly and assembly of thewing power system.

The aileron servo cabin is conve-nient to change the servo, sup-ports the installation of the air-speed meter module,shortensthe distance of the dynamicpressure tube, and improves theaccuracy of airspeed detection.(Optional) Left and right dualairspeed meter modules to improve the redundancy of air-speed.

The vertical tail and the fuselageadopt a 5-point integratedtoolless quick-release structure.

A 9-pin gold-plated connectoris used to realize the mechan-ical and electrical synchronousseparation of the tail and thefuselage.

The vertical tail servo can beflexibly disassembled and as-sembled for easy maintenanceand replacement.

The horizontal tail adopts a tool-less quick-release structure, whichis automatically locked with onepush and pulled out immediatelywith one push.

The left and right horizontaltail fins are designed with in-dependent control by dualservos, if either side fails, theaircraft can return homesmoothly, which improves thereliability of the aircraft.

The horizontal tail servo does notneed to be embedded in advance,which is convenient for the re-place of the servo.The servo rocker arm is designedwith built-in, even if the rockerdrive column is loose, the tailsurface can be executed precisely.