Makeflyeasy striver mini binary 2100mm UAV Fixed Wing

The wing and tail adopt tool-less quick disassembly structure to reduce the installation steps
and 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 isdesigned with a wire slot and aremovable baffle,it is conve-nient for the installation of thewires, and at the same time en-sures the concise and efficientwiring in the cabin.

The motor base of the machinehead is made of PC alloy plastic,which has strong impact resistance, 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 fuse-lage.

(Optional) 2-channel redundantflight control power supply in-tegrated in the power distribu-tion board, 1 way servo powersupply, 1 way load powersupply, shortened wire path,reduced soldering process,clean and tidy wiring

The hatch is reserved for the digi-tal transmission antenna holewhich is convenient to install andremove the antenna.

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

The auxiliary carbon tubeadopts a tool-less quick-release design, which is con-venient for carrying largerloads.
Reserved for common lenscutting holes, easy to openthe hole.

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

(Optional) Flight control protection cover to prevent foreignobjects from falling in,bothbeautiful and dustproof.

The GPS cabin is located at therear of the fuselage, the size of78x58x37 mm can place theflight control GPS and compassmodule, and the electromag-netic environment is clean.

The position of the PPK anten-na is reserved behind the GPScabin,it is convenient to instalPPK antenna to improve theaccuracy of POS data.

The size of the parachute cabinis 195x100x45mm,which canaccommodate 6-8kg parachute.
The lower opening design greatlyimproves the success rate of opening the umbrella.

The fuselage is reserved forparachute rope hooks, whichis convenient to fix the para-chute ropes, and the distanceis reasonable to increase thestability of landing.

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 connectors,realize 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 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 im-prove the redundancy of airspeed.

Pair text with an image to focus on your chosen product, collection, oThe vertical tail and the fuselageadopt a 5-point integratedtoolless quick-release structure.r blog post. Add details on availability, style, or even provide a review.

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 befexibly disassembled and assembled for easy maintenanceand replacement.

The horizontal tail adopts a tool-less quick-release structure,which is automatically locked withone push and pulled out immedi-ately with 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.