Performance
Community
Section | Item | SKYEYE-150 | SKYEYE-200 |
---|---|---|---|
Unit Part (Flight Vehicle) |
Cubic | 15 Cubic (15㎥) | 20 Cubic (20㎥) |
Size | 3.45m * 3.45m * 2.2m, Total Length 6.85m | 3.85m * 3.85m * 2.45m, Total Length 7.7m | |
Weight | 8kg | 9.5kg | |
Device | Automatic Pressure Regulator, Spitlight | Automatic Pressure Regulator, Spitlight | |
Mission equipment | Payload | 3kg | 5kg |
Size | Optional [Optical Zoom Camera (18x), Thermal/UV Camera] |
Optional [Optical Zoom Camera (36x), Thermal/UV Camera, Communication equipment, environmental collection sensor (climate sensor, etc)] |
|
Electric Winch | Size | 0.90 x 0.65 x 0.43 (m) | 0.90 x 0.65 x 0.43 (m) |
Weight | 65kg | 65kg | |
Maximum Winding Torque | 250kg/f | 250kg/f | |
Maximum Winding Speed | 53m/min | 53m/min | |
Helibase (Optional) |
Size | 3.3 x 2.7 x 1.7 (m) | |
Weight | 35kg | ||
Material | Stainless |
Section | SKYEYE | Drone(multi-rotor) | CCTV |
---|---|---|---|
Operating time | Constant Operation (periodic replenishment of helium (10days)) |
Within 30min |
365 days of regular operation |
Operating height | ~500m (Optimized height in actual operation : 150~300m) |
~150m (Restrictino of flight height due to legal regulations) |
1m ~ 15m (Requires separate structure) |
Dangerous Level | Low |
Very high |
Low |
Mobility | Great |
Good |
None |
Operating Condition | Available in rainy weatherAvailable even in high winds (within 22m/s) |
Unable to use in rainy weatherUnable to use eind dpeed of 10m/s or more |
Available in rainy weatherAvailable even in high winds |
Operating / Maintenance cost | Low Cost |
High cost |
Moderate cost |
Section | SKYEYE | Skyship |
---|---|---|
Operating Time | 365 days of operation(periodic replenishment of helium (7 days) |
Up to 6 hours (battery limit, flying time constraints) |
Environmental Impact in Operation | Available in rainy weather, the maximum wind speed, 22m/s |
Unavailable in rainy weather and over wind speed 10m/s Vulnerable to rain and wind due to wide flight vehicle operations Possible to lose control of flight vehicle and lose it during strong winds |
Flying Method | Helium gas buoyancy + Using the principle of kiteNo separate propellant |
Helium gas buoyancy + propeller propellant |
Mobility | Mooring type, limited mobility |
Securing mobility using propellant |
Operational personnel and features | 1 to 2 days of training for reliable operation |
Required flight control qualification Difficulty in securing space and maintenance according to the flight vehicle size Increase Management Operating Costs with Number of Operating Days |