| 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 |
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 | |||||||
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
|
||