UNITED KINGDOM
  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 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)
Aerobotics
Sprite
Underway    

 

 

 

 

 

 

 

Piston

 

 

 

 

 

 

 

 

 

 

 

Rotor = 5.3 13

 

 

 

 

10,000

 

15 2.0 No Tail; Counter-Rotating Rotors

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

BAE Systems
Ariel- Datalink decoy
Complete Underway Deployed

Airborne towed radar decoy. Relatively high power veision.

 EW suite.  Fully programable ECM, effective against monopulse, semi-active radars and home-on jamming systems; operates in H to J (6-20 GHz) frequency bands.

 Winched out on 200m cable  behind parent aircraft.

By cable reel-in on larger aircraft; with smaller aircraft, is jettisoned before landing and can be recovered by optional parachute system.

 

 

 

None

 

 

 

 

 

 

 

 

 

 100

 

   

 M 1.3

 

 

 

8,000

 

32 5.0  
 

 

In Royal Air Force

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

Ariel- RF-link decoy
Complete Underway Deployed

Able to take advantage of other EW equipment, such as an RWR or an ECM generator, etc.

 

 

 

 

None

 

 

 

 

 

 

 

 

 

 

 

   

 M 1.3

 

 

 

8,000

 

32 5.0  
 

 

In Royal Air Force

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 100

 

 

 

 

 

 

 

 

 

 

 

 

Phoenix
Complete Underway Deployed

Battlefield surveillance and target acquisition
UAV.

 IR payload with 360° scan azimuth.

Hycraulic/ pneumatic catapult installed on a six-wheel, 14 tone truck.

 

Parachute and airbag.

 Three GCS crews; nine other personnel

Air vehicles; one GCS; one ground data terminal; one launch vehicle; one launch support vehicle; one recovery vehicle; and one forward amintenance facility

 

One 25 hp Meggitt WAE 342 two-cylinder two-stroke engine.

Two-blade fixed-pitch wooden prop.

 5.50

 

3.80

 

 

 

 

 

 

 20

50 180

 85

 

 

 

8,000

 

38 4.5  
 

198 air vehicles were ordered and due delivery time by 2001.

In service from 1998. British Army (Nos 32 and 39 Regiments, Royal Artillery)

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

Channon
Nitro Hawk
Underway    

 

 

 

 

 

 

 

Piston

 

 

 

 

 

 

 

 

22

 

 

Rotor = 5 5

 

 

 

 

1,200

 

5 0.5 Helicopter

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

Cranfield Aerospace Ltd.
A3 Ovserver
Complete(?) Underway  

Close-range RSTA UAV

CCD TV cameras.

Bungee catapult launch

Automatic, by parachute and airbag or by belly skid landing.

 

 

UHF (400 MHz) uplink and D-band (1.2 GHz) downlink.

One 6.2 hp 88 cc BH88 two-stroke piston engine

Two-blade wooden pusher prop

2.40

 

 

 

 

 

 

 

 

 

4.0 30

>68

58

 

 

8,200

984

300-400 m 2  

First flight made on 11 March 1999.

 

UK Ministry of Defence

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

  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 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)
Cyberflight
 CyberOne
Underway    

Surveillance UAV

TV camera, night vision systems or communications relay packages.

Wheeled take-off

Wheeled landing

 

 

 

Two 2.5hp piston engines

Two two-blade prop

1.69

 

 

 

 

 

 

 

5.4

 

6.8  

87

 

31

 

20,000

 

17.5 >2  

First test flight in 1999

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

Swift-Eye
Underway    

Man-portable surveillance UAV

Colour TV camera; 35 mm film camera with normal or IR film

Hand-launch

Parachute for emergency recovery

 

 

UHF real-time imagery downlink

Single piston engine

Two-blade prop

1.42

 

 

 

 

 

 

 

1.8

 

  total system 6.4

83

 

26

 

14,000

2.500

1.7 >40 min  

First test flight in 1999

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

Supet Swift-Eye

Underway

 

 

 

 

 

 

 

 

 

Single piston engine

Two-blade prop.

1.52

 

 

 

 

 

 

 

2.3

 

 

 

83

 

26

 

14,000

2.500

1.7

>1.0

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

DPA
Watchkeeper
Underway / Assessment Stage 1    

Close-/ short-range intelligence surveillance, target acquisition and reconnaissance (ISTAR) UAV.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

   

 

 

 

 

 

 

     

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

Flight Refueling
Raven
Complete    

Close-range day and night surveillance UAV

CCD video camera

 By bungee- powered catapult

Skid landing or parachute recovery

4 cerws

A single support vehicle/trailer combination, comprising a GCS, launcher and air vehicles.

 

One 7 hp 200 cc Aerrow Quadra two-cylinder two-stroke engine

Two-blade pusher prop

3.66

 

3.175

 

 

 

 

 

 

9.3 (13.3 liters)

22 84

 97

60

55

 

14,100

600

54 >3.0  

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

  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 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)
Intora-Firebird
Firebird
Underway    

 

 

 

 

 

 

 

Tipjet

 

 

 

 

 

 

 

 

 

 

 

Rotor = 10 50

 

 

 

 

18,000

 

15 0.5 No Tail; Tip Jets

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

Meggitt
ASR-4 Spectre (Crecerelle)
Complete Underway Deployed

 Mulitirole UAV

 

 

 

 

 

 

One 25 hp Meggitt WAE 342 two-cylinder two-stroke

Two-blade fixed-pitch wooden pusher prop

 

 

 

 

 

 

 

 

 

 

   

130 

 

 60

 

9,840

 1,575

27 3.0 - 6.0  

With SAGEM france

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

ASR-4 Specte II
Complete Underway Deployed

Multirole UAV

 IAI Tamam POP TV/FLIR sensor

By free-standing or trailer- mounted bungee catapult; rocket- assisted take-off opteinal.

 By onboard parachute system, controled manually or automatically.

 Four personnel

Six air vehicles (tipically), one mobile GCS, one mobile launcher, support and spares equipment.

 

 One 38 hp UEL AR 741 rotary engine

 Two-blade fixed-pitch wooden pusher prop

3.28

3.72

2.74

0.97

 

 

 

 

 111.6

27.2 (40 liters)

25 144.7

 

 

 

 

22,965

 

86 3.0 - 6.0  

 

In service more than 60 with both surveillance and EW payloads.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

Phantom
Complete Underway

Available

Battlefield close-range reconnaissance and surveillance UAV

CCD video camera or IR. ECM and decoy systems optional.

By lightweight catapult.

Parachute recovery.

Typically, six air vehicles with electro- optical payloads, launcher, recovery and refurbishing equipment, and a command and control/ processing (C²P) unit. A single four-wheel drive vehicle provides complete system transport, air vehicle launch, flight control, real-time image interpretation and display.

 

One 8 hp 75 cc Zenoah two-cylinder two-stroke engine

Two-blade pusher prop.

 2.50

 

 1.52

 

 

 

 

 

23

9.5 liters

8.2 40

97

 

49

 

9,800

 

32.4 3.0  

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

  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 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)
Tasuma
CSV-20
Complete Underway Available

Close-range airborne surveillance system

Colour CCD TV camera or thermal imager

 From mobile trolley, JATO or lightweight catapult

Fuselage skid landing, or by on-command / fail-safe parachute.

 

 

 

One 38 cc single- cylinder two-stroke engine

Two-blade pusher prop.

2.85

 

2.47

 

 

 

 

 

 

 

10 20

76

 

40

 

5,000

 

4.3 2.0  

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

MSV-10
Complete    

 Ultra- lightweight surveillance UAV

CCD TV camera

 Hand- launched

 Fueslage skid landing or on-command/ fail-safe parachute

 

 

D-band (1.2 GHz) video

One 4 cc diesel engine

Two-blade prop

2.80

 

 1.70

 

 

 

 

9

 

 

  4.2

 

35

16

 

2,000

 

3 0.5  

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

UTS (Universal Target Systems Ltd)
Mercury
Underway    

Short-range UAV

 

Automatic, using existing systems, for which interfaces can be provided

Parachute recovery

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

11 30

 

apprx 78

 

 

 

 

  3.0