G25 VTOL Fixed Wing UAV Drone

Product Description

MD-25 drone shell, with the following main parameters:

Material: carbon fibre, glass fibre, Kevlar, PVC, etc.

Landing gear installation position: below the rotor shaft.

Mission bay position: directly beneath the aircraft’s centre of gravity.

Structural weight: approximately 3450g (including all structural and installation components).

Maximum take-off weight: 13.5kg.

Maximum payload: 3kg (standard load: 1.2kg).

Wing area: approximately 52dm².

Wing load: approximately 240g/dm² –12.5kg.

Endurance time: 3.67H (220min) –1kg load (measured near sea level in calm winds). Maximum control distance: manual control with remote control/approximately 0.5km-1km, ground station/5km-30km.

Standard cruising speed: 20m/s –12.5kg (operating speed of 21m/s –12.5kg is recommended for mountainous areas).

Maximum cruising speed: 93.6km/h (26m/s).

Standard battery configuration: 22.8v/25Ah*2 (45.6V).

Never exceed speed: 122km/h (approximately 34m/s).

Stall speed: 15.5m/s –12.5kg (16m/s –roll25°/pitch15°).

Minimum turning radius: 120m — 19m/s (roll 18°) (the safe turning radius in high-altitude areas is not less than 200m)

Maximum altitude for cruising: 4800m

Fixed-wing mode wind resistance: not less than level 6 wind (gusts up to level 7)

Rotor take-off and landing mode maximum wind resistance: not less than level 4 wind (gusts up to level 6)

Drone operating environment: -20℃ to 45℃; can fly in light rain (safe operating time greater than 10min)

Rotor emergency operation time: not less than 6.5min (when rotor battery is independently powered (non-standard power configuration))

Take-off and landing method: vertical take-off and landing

Vertical take-off propeller size: 16/17 inches (recommended)

Fixed-wing tail push propeller: 15 to 18 inches (recommended)

Fixed-wing maximum thrust-to-weight ratio: 0.6 (standard configuration)

High-altitude performance: has passed high-altitude testing (for high-altitude standard power configuration, please contact the manufacturer)

Standard empty take-off weight: approximately 11.5kg

Safe voltage when entering the descent flight path: not less than 44V (Gens high-pressure version battery)

Wing installation angle: 2°

Number of airspeed tube installations: 2 (the standard is a single airspeed tube opening)

Does the system support non-stop power battery replacement: yes (non-standard)

Flight control support type: flight controls that support compound wing control can be used for this model of drone system”Solid-state” battery endurance: 4.35H (261min) — no load (measured near sea level in calm conditions)