|
Other East EUROPE |
|
|
country
|
Prime Manu.
|
UAV Designation
|
Production status
|
Operational status
|
Power plants
|
Dimensions (m)
|
Wieghts
|
Performance
|
Comments
|
||||||||||||||||||||||||||
|
Development
|
Production
|
Operation
|
Purpose
|
Mission payload
|
Launch, take-off type
|
Recovery, landing type
|
Min ground crews need
|
System composite
|
Datalink, comm frequency
|
Engine
|
Propulsion
|
Wing span
|
Wing area (§³)
|
Length overall
|
Height overall
|
Wheel track
|
Wheel base
|
Wing aspect ratio
|
Fuselage max width
|
Weight empty
|
Max fuel weight
|
Max Payload
|
Max T-O/launch weight
|
Max level speed (kt)
|
Cruising speed (kt)
|
Loiter speed (kt)
|
Stall speed (kt)
|
Service Ceiling (ft)
|
Max rate of climb (ft/min)
|
Range (nm)
|
Max Endurance (h)
|
||||
|
Bulgaria
|
Aviotechnica
|
Yastreb-2S
|
Complete | Complete | Deployed | Recoverable airborne jammer | AJ-045A radio jammer | HF/VHF(18 to 104 Mhz) | One 16.5 hp DB-250 two-stroke engine | Two-blade propeller | 3.52 m | 2.85 m | 0.533 m | 4.5 kg | 66 kg | 97 | 86 | 5,905 | 27 | 1.5 | |||||||||||||||
| flight test mid-1994 | Army | ||||||||||||||||||||||||||||||||||
|
Poland
|
OBRUM
|
Bee
|
Underway | Micro UAV | Reconnaissance sensor. | Hand launched | Belly landing. | LOS radio control | One Cox Tee Dee .01 ;istion engine initially. | 0.635 | 70 g | 170 g | 27 / 32 (target) | 10 min / 20 min (target) | |||||||||||||||||||||
| serveral test in 2000. | |||||||||||||||||||||||||||||||||||
|
CamBat
|
Underway | Underway | Very close-range mini-UAV. Offered to Polosh Police in mid-2000. | Recon / Surveil sensor. | Fron roof of small mobile control vehicle. | Wheel or belly landing. | RC control | Electric motor. | 2.0 | 0.3 | 1.7 | 21.5 | 5.4 / 13.5 (target) | 15 min / 40 min (target) | |||||||||||||||||||||
| Prototype flown | |||||||||||||||||||||||||||||||||||
|
Portugal
|
IST/OGMA
|
ARMOR X7
|
Complete(?) | Underway | Civil research programme. | TV or LLTV camera or FLIR sensor. | Wheeled take-off. | Wheeled landing; parachute for emergency. | Twin piston engine. | A single two-blade pusher prop. | 6.0 | 3.60 | 3.575 | 1.425 | 1.475 | 1.135 | 50 | 200 | 54 | 6,600 | 216 | 12-15 | Teamed with IST | ||||||||||||
| Development programme said to be nearing completion in second quartor of 2000. | |||||||||||||||||||||||||||||||||||
|
Yugoslavia
|
SDPR
|
VBL-2000
|
Underway(?) | Mulitipurpose UAV | Day TV camera. AF camera, IRLS or EW/ECM. | Wheeled take-off, or platform- launched by solid propellant rocket booster. | Wheeled (optionally skid) landing. Parachute recovery abailable in both cases. | One pistron engine. | Shrouded pusher propeller. | 3.30 | 3.25 | 1.22 | 30 | 30 | 150 | 100 | 74 | 11,975 | 721 | 594 | 8 | ||||||||||||||
| 1990 | |||||||||||||||||||||||||||||||||||
|
|
|
|
|||||||||||||||||||||||||||||||||