KOREA
(Undated July 21. 2007)
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KOREA
(Undated July 21. 2007)
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Prime Manu.
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UAV Designation
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Production status
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Operational status
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Power plants
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Dimensions (m)
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Wieghts (kg)
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Performance
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Comments
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Development
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Production
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Operation
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Purpose
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Mission payload
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Launch, take-off type
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Recovery, landing type
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Min ground crews need
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System composite
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Datalink, comm frequency
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Engine
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Propulsion
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Wing span
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Wing area (§³)
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Length overall
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Height overall
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Wheel track
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Wheel base
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Wing aspect ratio
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Fuselage max width
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Weight empty
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Max fuel weight
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Max payload
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Max T-O/launch weight
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Max level speed (kts)
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Cruising speed (kts)
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Loiter speed (kts)
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Stall speed (kts)
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Service ceiling (ft)
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Max rate of climb (ft/min)
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Max range (nm)
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Max endurance (h)
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KAI
(Korea Aerospace Industries, Ltd.)
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ARCH-50
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Complete |
agricultural unmanned helicopter. |
Hopper/tank and spray or spreader kits for agricultural chemical. |
Conventional helicopter take-off. |
Conventional helicopter landing. |
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One 65 hp Rotax 586 Two-cylinder two-stroke water-cooled engine. |
Two-stage bevel gear transmission. |
Rotor dia= 4.80 | 1.30 | 238 | 14 liters | 50 | 300 | 54 | IGE 330 | 1,312 | 0.5 | |||||||||||||
| Since 1992. |
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TRPV-1 Doyosae
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Complete |
Reconnaissence and surveillance UAV. |
LG Autoboy still-film camera. XSR-1 dual-sensor. |
Conventional wheeled take-off. |
Conventional wheeled landing. |
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One 28 UEL AR 731 rotary engine. |
Two-blade fixed-pitch pusher prop. |
4.80 (prop dia= 0.66) | 2.84 | 3.52 | 2.0 | 1.0 | 1.17 | 113 | 15 (40 liters) | 0.5 | 130 | 6,000 | 27 | 3.0 | |||||||||||
| Since 1991. |
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| Complete |
Completed |
Deployed |
Reconnaissence and surveillance UAV. Short range tactical UAV. |
Daylight TV/ FLIR sensors |
Conventional wheeled take-off; optionally from truck mounted hydraulic/ pneumatic catapult launch. |
Conventional wheeled landing; parafoil for emergency recovery. |
20 |
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UHF/C-band |
One 38.8 kW(52 hp) UEL AR 801R rotary engine,
driving a four-vlade fixed-pitch wooden pusher propeller.
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6.4 | 4.80 | 1.47 | 215 | 45 | 300 | 65-67 | 15.000 | 65 / 108 with relay | 6.0 | ||||||||||||||
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Durumi
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Cancled |
Long-endurance research prototype. |
Miniature CCD camera with two-axis stabilisation. |
Conventional wheeled take-off for test flight; launched from car roof-fack for long-endurance performance. |
Conventional wheeled landing for test flight; belly landing for long-endurance performance. |
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E/F-band control uplink with UHF back-up. |
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0.15 | 0.69 | The development for meteorology research purpose mission is on going. METRI, UAVCENTER, Uconsystem were joined in this program. | ||||||||||||||||||||||
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Since 1999. |
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Smart UAV |
Underway |
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High speed, light weight smart VTOL UAV. |
Optional, as required. |
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Since 2002. |
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1~3 (m) |
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300 (kg) |
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500 (km/h) |
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5 hours |
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CAMCOPTER S-100 |
Complete |
Underway |
Deployed |
Multiful Reconnaissence and surveillance Auto-VTOL UAV. Short range tactical UAV. (Corps, Division and Brigade operation level) |
EO/IR(basic), SAR, Ranger designator, NBC detector etc(optional), Agricultural spry device and movie camera. |
Full Auto Vertical Take-off |
Full Auto Vertical Landing |
3 |
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C-band/UHF |
One single-disc 55 hp Rotary Engine with FADEC(Full Authority Digital Engine Control). |
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main rotor dia: 3.40, tail rotor dia: 0.66 |
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Fuselage: 3.20 |
0.704 |
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0.50 |
100 |
41 |
60< |
200 |
120 |
100 / max 130 |
55-65 |
N/A |
18,000 at 138 kg |
2000 at 180kg, 4000ft altitude |
265 ~ 384. Nomal 100 |
6.0 at full fuel and 25kg payload |
Helicopter |
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OEM Schiebel Austria |
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Hover Ceiling: 15,600ft/120kg 6,400ft/200kg |
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CAMCOPTER 5.1 |
Complete |
Underway |
Deployed |
Multiful Reconnaissence and surveillance Auto-VTOL UAV. Close range tactical UAV. (Regiment and Battalion operation level) |
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C-band/UHF |
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OEM Schiebel Austria |
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Prime Manu.
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UAV Designation
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Production status
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Operational status
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Power plants
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Dimensions (m)
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Wieghts (kg)
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Performance
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Comments
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Development
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Production
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Operation
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Purpose
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Mission payload
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Launch, take-off type
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Recovery, landing type
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Min ground crews need
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System composite
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Datalink, comm frequency
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Engine
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Propulsion
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Wing span
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Wing area (§³)
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Length overall
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Height overall
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Wheel track
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Wheel base
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Wing aspect ratio
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Fuselage max width
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Weight empty
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Max fuel weight
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Max payload
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Max T-O/launch weight
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Max level speed (kts)
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Cruising speed (kts)
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Loiter speed (kts)
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Stall speed (kts)
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Service ceiling (ft)
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Max rate of climb (ft/min)
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Max range (nm)
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Max endurance (h)
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Underway |
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Prototype |
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Underway |
Underway |
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Under prototype testing |
Prototype |
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Undeway |
Underway |
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Under prototype testing |
Prototype |
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Underway |
Underway |
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Under prototype testing |
Prototype |
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Underway |
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Under prototype testing |
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