GERMANY
Country
  
Prime Manu.
UAV Designation
Production status  
Operational status          
Power plants
Dimensions (m)            
  Wieghts (kg)    
      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)
 
Eurodrone (Franch (Matra BAe Dynamics) & German (MBB) international)
Brevel/ Tucan
Complete Underway Deployed

 First two complete operational units (each with five airvehicles) were delivered for operational evalution by the French and German armed forces in April 1998; nearly 200 flights made by mid-1999.

Reconnaissance, target location/ designation and damage assessment UAV

Zeiss Ophelios 12 micron stabilised day/night (FLIR) sensor.

 Jettisonable booster rocket.

Parechute and airbag recovery system. 200 × 200 m needed.       One two-cuylinder two-stroke engine. Two-blade pusher prop. 3.42   2.28 0.96             35 161  135 81 65   13,200   81 3.5  
                                                               
 

EADS Dornier

DAR
Complete Complete Deployed Lethal or non-lethal target engagement. Can include active (MMW) or passive (anti-radar) sensor/ seeker, VHF jammer(high power), anti-jammer, laser and IR sensors, elint systems and fragmaentation warhead, depending upon mission. Container-launched by single-chamber rocket booster from zero-length rail. Parachute and net recovery systems optional for non-lethal missions.     Real-time One 27.5 hp(at 7000rpm) 352 cc Fichtel and Sachs SF 2-350 two-cylinder two-stroke engine. Two-blade pusher prop (dia: 0.67 m). 2.0   2.30 0.36           18 70 120 135       9,800  980 >81 >3.0 Truck mounted container can accommodate up to 18 air vehicles and can be sealed for long-term storage.
                                                               
 
EADS Dornier
Seamos
Complete   2006 - 2008 Maritime recommaissance and target acquisition VTOL UAV. Multimode sea surveillance radar and an EO/IR sensor. Conventional helicopter take-off (automatic). Conventional helicopter landing (automatic).       One 450 shp Rolls-Royce  250-C20R/ 1S turboshaft.   Dia: 6.10   2.89  2.50       1.50    350 180 1,125 90 55-80     12,000 980 110 4.7 No Tail; Counter-Rotating Rotors
                                                                 
 
Ceselsa/ INTA (Spain)/ EADS Dornier (Germany)
SIVA
Complete Underway   Surveillance UAV IAI Tamam Moked 400 FLIR/ CCD TV; IRLS module. OKT Norge 10/150 hydraulic catapult, or two booster rockets. Parechute system. Twin under fuselarge airbags cushion landing impact.   GCS Real-time datalink E-band (2.2-2.4 GHz) One 26 hp Sachs SF2-350 two-cylinder two-stroke engine -> 49.6 hp Rotax 503 UL flat-twin. Two-blade fixed-pitch prop. 4.828 3.33 3.78 0.95       0.42 160 40 30 230 102 76     9,800 669 81 10  
                                                                 
   
Prime Manu.
UAV Designation
Production status  
Operational status          
Power plants
Dimensions (m)            
  Wieghts (kg)    
      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)
 
EMT
Luna X-2000
Complete Underway Deployed Close-range battlefield RSTA UAV. Daylight CCD colour TV camera, Zeiss P286D Attica non-stabilised, 1.7 kg thermal imager in ventral bay, miniature SAR. From 4 m rail by EMT bungee catapult, foldable for trnsport. Parachute recovery system standard.   GCS Real-time, HF (5MHz) uplink, UHF data downlink/ G-band (5GHz) One 6.7 hp two-cylinder two-stroke engine with restart capability. Three-blade pusher prop with folding blades. 4.17   2.24 0.78         20   3 30  86  38  26   9,800  980 43 (real-time) / >54 3.0  
    Two platoons were deployed to Prizren, Kosovo on 27 March, and on April 2000.                                                            
 
IAT  
MK-105 Flash
Complete                   Piston                                   10,000   27 3.0  
                                                                 
MK-106C Hit
Complete                   Piston                                   12,000   27 3.0  
                                                                 
 
STN Atlas
Taifan/ Mücke
Underway   2003 Attack (Taifun) and ECM (Mücke) UAV High-resolution K-band (¡Ö 35 GHz) MMW radar seeker with MTI capability. Booster rocket Taifun non-recomerable; Mücke parachute and airbag recovery system.       One 43 hp two-cylinder two-stroke heavy-fuel engine. Two-blade wooden pusher prop. 2.26   2.08 1.04             50 160 108   65   >13,200   54 4.0  
                                                                 
 
TESTEM
Deltron III
Underway                   Rotary                                   13,000   27 3.0 Rotor in Wing