SPECIFICATIONS
Brand Name: NoEnName_Null
Origin: Mainland China
Material: Foam
Recommend Age: 14+y
Use: Vehicles & Remote Control Toys
new generation of aerial surveying hand-thrown fixed wing inherits safety and practical characteristics of the Fighter . MFE team has made effort to repeatedly polish in the fields of flight stability, power configuration, and quick release and portability .
ic Parameters Material: EPO, EVA, carbon fiber, engineering plastics, etc. Wing area: 59dm? Maximum takeoff altitude: SOOm(altitude)
the Striver mini optimizes the aerodynam- ic shape and relative position of the wing, tail, vertical tail, and fuselage . the increase of lift force reduces the drag significant- ly, and the flight efficiency is high .
embedded box structures are used to com- prehensively improve the structural strength and rigidi- ty of the body . on the basis of "overload ex- periment"
Hand Throw Takeoff The fuselage tail hand grip size and hands to hold the aircraft power spacing to achieve accurate power and smooth throwing: J0" 5-9: 50" 70" i0. #(:cm 75cm Sing I e/ dua| motor compatible.
the wing and tail adopt tool-less quick disassembly structure to reduce the installation steps and shorten the assembly time . the inner liner of the packing box is made of high-magnification EPS foam .
the inside of the fuselage is designed with a wire slot and a removable baffle . it is conve- nient for the installation of the wires and at the same time en- sures the concise and efficient wiring .
motor base of machine head is made of PC alloy plastic, which has strong impact resis- tance . ESC adopts a built-in design, and the maximum supported size is 71x38mm .
battery holder is made of PC board CNC processing, which is light in weight and has good impact resistance . the battery ties have a reasona- CELLS 77 ble layout; which is convenient 88.#Wh for binding and unbinding .
the hatch is reserved for the digi- tal transmission antenna hole, which is convenient to install and remove the antenna . the hatch has a shortened wire path, reduced soldering process, clean and tidy wiring .
the auxiliary carbon tube adopts a tool-less quick- release design, which is con- venient for carrying larger loads_ Reserved for common lens cutting holes, easy to open the hole_
the flight control cabin adopts a platform-based open design, compatible with ope source/commercial flight control installation 8] . the center panel can make full use of the space @HH layout; extremely .
the cabin is located at the itaoglas rear of the fuselage . the position of the PPK anten- na is reserved behind the GPS cabin,it is convenient to install PPK antenna to improve the accuracy of POS data.
the lower opening design greatly improves the success rate of ope- ning the umbrella . the fuselage is reserved for parachute rope hooks, which is convenient to fix the para- chute ropes .
the and fuselage are customized industrial-grade 9+2 high-current connectors . the hinge connects the aileron to increase the accuracy and durability of the execu- tion .
wing motor base adopts an embedded box structure to connect with the main carbon tube of the wing . the motor base supports the maximum outer rotor diameter 044mm motor .
the aileron servo cabin is designed in the middle of the wing to facilitate the installation of ESC wires . the air- speed meter module is installed in the cab to shorten the distance of the dynamic pressure tube .
a 9-pin gold-plated connector is used to realize the mechan- ical and electrical synchronous 0 separation of the tail and the fuselage . vertical tail servo can be flexibly disassembled and as- sembled for easy maintenance and replacement .
the horizontal tail adopts a tool- less quick-release structure, which is automatically locked with one push and pulled out immediately with one . the left and right horizontal tail fins are designed with in- dependent control by dual servos, if either side fails, the aircraft can return home smoothly .
LUAAtulUium? :uRisa* 14-8+4#0RA183n5# document before installing . most of the information you need is here_ D0X LiAAAuin5_0434L 4Uz* 7i EE aFreeman?-IANTOL MALAt .
4+1 mode wiring diagram left front Front pull Right fron moto motor 5oo8kv380 6582200mah ESC ESC Airspeed 40A 80A 40A Airspeed meters 12C1 meter 12C2 AB M3 5V ScL1 SDA1 Sv SCLZ SDAZ BEC 5V 10A M5 Left aileron Right aileeron ervo servo ES 3054 ES3054 Left ctor Camera shutter cable/(13
make sure that the aircraft is far away from crowds and dangerous objects when flying . do not carry out aircraft operation while drinking, fatigue or mental discomfort .