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 features an aerodynamically optimized design, where the wing, tail, vertical tail, and fuselage are carefully positioned to maximize lift while minimizing drag. This results in a significant reduction of air resistance, leading to high flight efficiency.

The mini Striver’s robust structure utilizes embedded box structures to comprehensively enhance its overall strength and rigidity, as verified through rigorous overload testing.

For hand-throw takeoff, the fuselage tail and hand grip design allow for easy handling and accurate power control. The aircraft’s power spacing is optimized to achieve smooth throwing and precise flight performance. It measures 50cm to 70cm in length and has a wingspan of 75cm, making it compatible with single-motor configurations.

The mini Striver features a innovative tool-less quick-disassembly design for its wings and tail, allowing for rapid installation and reduced assembly time. Additionally, the inner lining of the packing box is crafted from high-magnification EPS foam for enhanced protection and storage efficiency.

The interior of the fuselage features a wire slot and removable baffle, allowing for convenient installation of cables while ensuring concise and efficient wiring.

The motor base of the machine head is constructed from durable PC alloy plastic, offering excellent impact resistance. The ESC features a built-in design, with a maximum compatible size of 71mm x 38mm.

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 designed with a convenient digital transmission antenna installation/removal feature. Additionally, it features a compact wire path that simplifies the soldering process, resulting in neat and organized wiring.

The auxiliary carbon tube features a tool-free quick-release design, allowing for effortless handling of heavier payloads. Additionally, it has reserved lens cutout holes that can be easily opened.

The flight control cabin features an open platform-based design, allowing for seamless integration with both open-source and commercial flight control systems. The central panel takes full advantage of its available space, offering an @HH layout that is 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 unique lower-opening design enhances the efficiency of deploying the drone’s propellers. Meanwhile, the aircraft’s fuselage features dedicated attachment points for parachute ropes, simplifying the process of securing them.

The aircraft features customized industrial-grade 9+2 high-current connectors on the fuselage, while the hinge design ensures accurate and durable connection between the aileron, enhancing overall performance.

The wing motor base features an integrated, rectangular design that connects seamlessly to the primary carbon fiber wing spar. This configuration provides support for the maximum outer rotor diameter of up to 44 mm.

The striver mini’s aileron servo compartment is strategically located at the center of the wing, allowing for convenient installation of ESC wiring. Additionally, the airspeed meter module is integrated into the cabin to minimize the distance between the dynamic pressure tube and reduce overall system complexity.

A gold-plated connector with nine pins enables synchronized mechanical and electrical connections between the tail and fuselage, allowing for seamless separation and reassembly. The vertical tail servo can be easily disassembled and reassembled for simple maintenance and replacement.

The horizontal tail features a tool-less quick-release mechanism that automatically locks into place with a single push and can be easily released immediately with another push. Additionally, the left and right horizontal tail fins are independently controlled by dual servos, allowing the aircraft to return home safely in the event of a failure on one side.

Product information: Before using this aerial survey carrier (fix-wing UAV aircraft), read the manual carefully and refer to the instruction document for detailed setup and installation procedures.

Four-Mode Wiring Diagram: Front-left, Front-right Motor Wiring Diagram; 5008KV380 ESC with 6582200mAh Battery, Airspeed Meters (40A/80A), Temperature Sensor (12C1/12C2), and Other Components (M3, SDA1, SV, SCLZ, SDAZ, BEC, 5V/10A); Left Aileron, Right Aileron Servo ES3054; Camera Shutter Cable.

Striver Mini Spare Parts Kit (Hand Launch Configuration): Left Wing Assembly Specification

Ensure the drone operates at a safe distance from crowds and hazardous obstacles during flight. Additionally, refrain from operating the aircraft while under the influence of alcohol, fatigued, or experiencing mental discomfort.