Makeflyeasy Striver Mini Hand Version

Makeflyeasy Striver mini (Hand Version) Basic parameters Material: EPO, EVA, carbon fiber, engineering plastics, etc. Wingspan: 2100mm Fuselage height: 156mm (without foot pads) Fuselage length: 1200mm Wing area: 59dm2 Disassembly method: tool-less quick disassembly Load ...Makeflyeasy Striver mini (Hand Version) Basic parameters Material: EPO, EVA, carbon fiber, engineering plastics, etc. Wingspan: 2100mm Fuselage height: 156mm (without foot pads) Fuselage length: 1200mm Wing area: 59dm2 Disassembly method: tool-less quick disassembly Load compartment size: 180×150×110mm Transport box size: 1.08×0.35×0.48m Payload Max.

payload: 1.2kg Max. take-off weight: 7kg Flight Take-off and landing method: hand-throw parachute landing Maximum takeoff altitude: 5000m Practical altitude: 6000m Wind resistance: Class 5 (normal operation) Cruising speed: 17-20m/s Stall speed: 10m/s (altitude 500m, takeoff weight 6kg) Maximum range: 200km (battery 6S@30000mah, load 600g ) Range performance: 145min/150km (speed 18m/s, load 600g, battery 6S@22000mah, takeoff weight 6kg, altitude 500m) SPECIFICATIONS Brand Name : NoEnName_Null Origin : Mainland China Material : Foam Recommend Age : 14+y Use : Vehicles & Remote Control Toys STRIVER MINI HAND THROW Striver mini hand throw is a new generation of aerial survey fixed wing, it inherits the safe and practical qualities of Fighter, the MFE team has made every effort to repeatedly polish in the field of flight stability, power configuration, quick disassembly and portability, in pursuit of aerial artwork that can withstand the test of time. 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