UNMANNED HELICOPTER
Take-Off Weight
360 KG
Payload
250 KG
Altitude
6000 M
Endurance
8 Hours+
MK-400
Mk-400 is the heavy duty model in the Master Key series of UAVs. It has maximum take-off weight of 360kg，and other countless of advantages, such as high flying speed, heavy loading ability, long endurance, etc. Its performance is better than other products in 400-500kg take-off weights.
Mk-400 equipped with a turboshaft engine，and use heavy-fuel. Tandem layout with foldable design makes Mk-400 fits IATA standard. A standard P6P/PMC aircraft pallet can carry 2-3 Mk-400 and all ground devices, greatly enhanced the portability of the system and reducing the time of system expansion and recovery.
Modular operation and maintenance
- High autonomy and control capabilities
- No human intervention required throughout the operation
- Short training time for users (average of 15 days)
- Single-person mission operation
- Night flying capability
- Accurate lifting in unknown environments
Product Specification
| Features | Specs |
|---|---|
|
Rotor diameter |
3460 mm
(136.22 inches） |
|
Fuselage length |
2550 mm
(100.39 inches） |
|
Fuselage width |
890 mm
(35.04 inches） |
|
Height |
1023 mm
(40.28 inches） |
|
Cruise speed |
150 km/h
(93.2 mph) |
|
Maximum speed |
200 km/h
(124.3 mph) |
|
Wind resistance |
Up to 60 km/h |
|
Power system |
Turbo-shaft Engine |
|
Fuel |
Jet A, Kerosene, Diesel |
|
Takeoff weight |
360 kg
(793.66 lb) |
|
Payload |
250 kg
(551 lb) |
|
Endurance |
8 hours+ with auxiliary fuel tank |
|
Service ceiling |
6000 m
(19,685 ft) |
|
Mission ability |
3 hours @ 150kg (330.69 lb) payload 1.8 hours @180 kg (396.83 lb) payload |
A standard P6P/PMC aircraft pallet can carry 2-3 Mk-400 and all ground devices, greatly enhanced the portability of the system and reducing the time of mission tasking and recovery.
Master Key (MK) Series Category
| Features | Specs |
|---|---|
|
Cruise speed
|
150km/h
|
|
Takeoff weight
|
360kg
|
|
Paylaod
|
250kg
|
|
Wind resistance
|
Up to 60km/h
|
|
Endurance
|
8h+
|
|
Fuselage length
|
2550mm
|
|
Fuselage width
|
890mm
|
|
Height
|
1023mm
|
| Features | Specs |
|---|---|
|
Cruise speed
|
150km/h
|
|
Takeoff weight
|
286kg
|
|
Paylaod
|
166kg
|
|
Wind resistance
|
Up to 60km/h
|
|
Endurance
|
12h+
|
|
Fuselage length
|
2410mm
|
|
Fuselage width
|
890mm
|
|
Height
|
1230mm
|
| Features | Specs |
|---|---|
|
Cruise speed
|
150km/h
|
|
Takeoff weight
|
60kg
|
|
Paylaod
|
37kg
|
|
Wind resistance
|
Up to 60km/h
|
|
Endurance
|
3h
|
|
Fuselage length
|
1450mm
|
|
Fuselage width
|
650mm
|
|
Height
|
630mm
|
| Features | Specs |
|---|---|
|
Cruise speed
|
90km/h
|
|
Takeoff weight
|
18kg
|
|
Paylaod
|
12kg
|
|
Wind resistance
|
Up to 45km/h
|
|
Endurance
|
60min
|
|
Fuselage length
|
995mm
|
|
Fuselage width
|
505mm
|
|
Height
|
430mm
|
Aluminum alloy skin structure
- Overall weight reduced
- Superior weather resistance and corrosion free low cost and simple maintenance
- Good electromagnetic compatibility
Fully articulated rotor head structure
- Excellent resistance at high wind speed up to 60km/h.
Longer lifespan
High reliability
Maintenance cycle is over 200 hours
Simple operation, one click to complete the mission. Easy operation and modular maintenance on risk.
- High autonomous and control capabilities
- No human intervention is required throughout the mission
- Short training time for users (average of 15 days)
- Single-person mission operation
- Night flying
- Capable
High Reliability and Environmental Adaptability Turbine Shaft Engine
- Compact dimensions and lightweight
- Maintenance interval of 200 hours
- Time Between Overhauls (TBO) of 1000 hours
- Fully electronic control, environmentally adaptable
- Multi-fuel adaptability (aviation kerosene, diesel, jet fuel)
