SJW-2 Gyroplane

The SJW-2 has a short takeoff distance and no special requirements for runways

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SJW-2 Gyroplane

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Product Description

The SJW-2 has a short takeoff distance and no special requirements for runways

It can take off and land within a very short distance of 0-70 meters. The rotorcraft has only 2 blades on top, but can fly in the sky at a height of several dry kilometers. It can resist strong winds and turbulence up to 80 km/h, and can land safely at 10-130 km/h, even if the engine is off. It can take off and land as long as it is on a public wide platform or on a road.

Data sheet of Phoenix gyro plane
1 Dimensions(no rotor): 5.10×1.90×2.70 M(L x W x H)
2 Main rotor diameter: 8400 mm
3 Engine: ROTAX 912 100 horsepower
4 Empty weight: 280 kg (DS-115)
5 Maximum take off weight: 495 kg (DS-115)
6 Flight speed: 38 km/h - 185km/h  140km/h (cruise)
7 Maximum air route distance: 500 km / 1000 km (add auxiliary fuel tank)
8 Maximum flight altitude: 3500 m(no payload)(cruise)
9 Maximum payload: 160 kg(full fuel)  188 kg(half fuel)
10 Maximum hover time: 30 S (low to wind level 3)
11 Continue climbing speed: 5 m / s
12 Distance of takeoff run: 80 m
13 Distance of landing run: 130 m
14 Fuel capacity: 68 L
15 Operating temperature: -30°C to 50°C
16 Level of wind resistance: sustaining wind level 9( the best advantage of gyro plane)
17 Data & image transform distance: as need (30km 50km 100km)
18 IP protection: IP 4 (can improve later)
19 Battery
on board
Voltage: 12V
Capacity: lead battery 14000 mAh
Charge style: Self-charging in flight
20 Duration of flight Fuel tank full 68 L: Payload 0kg:about 4.5 hours
(Sea level, ambient temperature 20℃)
21 Modification list:         WHATEVER pod (HD/IR/laser)
Data & image transform as need
High-precision RTK
Handheld remote control with screen for automatic pilot
Auxiliary fuel tank
Weapon pylon
These modification above need pay more
22 Economical efficiency 230 CNY each flight hour

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