| 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)
|
| |
AD & D
|
Hornet
|
Complete |
Underway |
|
VTOL UAV |
|
Vertical take-off. |
Vertical landing. Parechute for emergency. |
|
GCS |
|
Four 22 hp Hirth F33-15A single-cylinder piston engines. |
|
Dia 2.20 |
|
|
2.30 |
|
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|
|
145 |
|
|
260 |
40 |
|
|
|
IGE 8,000; OGE 5,000 |
|
|
30 min |
|
| |
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| |
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Aerolight
|
Complete |
Underway |
Deployed |
Over the hill, Reconnaissance and Surveillance.
Border Patrol and Coast Guard.
Forest fire control and monitor.
Law enforcement missions.
Training system for Hi-End UAV systems operators.
|
PTZ camera
Sensor: Optical
Supplied by world leading companies.
|
Conventional wheeled take-off. |
Conventional wheeled landing. |
|
3 Aerolight Air-Vehicles with UMASTM avionics Mission.
Control Station -
Launch & Recovery Station - Optional.
Remote Payload Operation Terminal.
Ground Data Terminal.
Payload.
Integrated Logistics Support.
|
|
One 6-11 hp piston engine |
Two-blade pusher prop |
4.0 |
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8 |
40 |
|
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10,000 |
|
27 |
5 |
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 |
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Aerosky
|
Complete
|
Underway
|
Deployed
|
Applications:
Close range day and night,
Reconnaissance and Surveillance.
Target acquisition and designation.
Border Patrol and Coast Guard.
Forest fire control and monitor.
Law enforcement missions.
Training system
|
Stabilized pitch & yaw gimbals.
Sensor: Day/Night Electro-Optic/Infrared.
Supplied by world leading companies.
|
|
|
|
3-6 Aerosky Air-Vehicles with UMASTM avionics.
Mission Control Station.
Launch & Recovery Station.
Optional Remote Payload Operation Terminal.
Ground Data Terminal.
Payload.
Integrated Logistics Support.
|
|
one 15-20 hp piston engine |
|
4.50 |
|
|
|
|
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|
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|
18 |
70 |
|
|
|
|
15,000 |
|
54 |
>5 |
Integrated Logistic Support:
Full operation,maintenance and technical documentation.
Ground support equipment and spare parts package.
Comprehensive class room and field training.
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Aerostar
|
Complete
|
Underway
|
Deployed
|
|
|
|
|
one 26-32 hp piston engine |
|
6.20 |
|
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50
|
200 |
|
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18,000 |
|
Up to 108 |
>10 |
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Tail Sitter
|
Underway
|
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|
VTOL tactical UAV
|
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|
2 RF command uplinks and real-time imagery
down-link.
|
40 HP
|
|
10 ft (3m)
|
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6.6 ft (2m)
|
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33 Ib (15kg)
|
220 Ib (100kg)
|
150 Kt
|
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|
22,000 ft
|
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|
3
|
Guidance:
UMASTM avionics: real time UAV and payload control
Full autonomous navigation and in-flight
programmable navigation
Cemera guided navigation.
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| |
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)
|
| |
BTA
|
Canard
|
Underway |
|
|
Surveillance and target acquisition UAV. |
Day TV camera; as required. |
Conventional wheeled take-off; bungee catapult launch optional.
|
Conventional wheeled landing; parachute recovery optional.
|
|
|
|
One 100 cc two-stroke piston engine. |
Two-blade pusher prop |
2.40 |
|
1.90 |
|
|
|
|
|
|
|
7.9 |
40 |
80 |
|
50 |
|
12,000 |
|
27-54 |
6.0 |
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| |
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Mini Sheddon
|
Complete |
|
|
Multirole short-range UAVs. |
Day TV camera; as required. |
Conventional wheeled take-off; bungee catapult launch
optional. |
Conventional wheeled landing; parachute recovery optional.
|
|
|
|
One 75 cc two-stroke piston engine. |
Two-blade pusher prop |
3.0 |
|
2.0 |
|
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|
|
9.8 |
27 |
70 |
|
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|
12,000 |
|
5.5-27 |
2.5 |
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Sheddon MK3
|
Complete
|
|
|
//
|
//
|
//
|
//
|
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|
|
One 100 cc two-stroke piston engine. |
//
|
4.20 |
|
2.60 |
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40 |
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15,000 |
|
27-54 |
6 |
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| |
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| |
EAS
|
Crow
|
Complete |
Limited |
Limited |
|
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|
Piston |
|
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16.8 |
55 |
|
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15,000 |
|
108 |
9.0 |
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Vanguard
|
Complete |
Underway |
Limited |
|
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Piston |
|
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19.7 |
88 |
|
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|
15,000 |
|
108 |
16.0 |
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| |
EMIT
|
Sting ¥°
|
Complete |
Underway |
Deployed |
Long-endurance surveillance UAVs. |
IAI Tamam POP. |
Bungee launch or wheeled take-off. |
Parachute recovery, or wheeled landing with arrester hook
and cable. |
|
GCS/GDT |
|
One two-cylinder piston engine. (25 hp Meggitt WAE 342 two-stroke
in Blue Horizon.) |
Two-blade pusher prop. |
|
|
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|
60 liters |
400 |
|
|
60 |
|
|
18,000 |
|
81 |
48 |
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| |
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Sting ¥±
|
Complete
|
Underway
|
Deployed
|
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|
35 |
|
|
78 |
|
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|
24 |
|
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Blue Horizon 2
|
Complete
|
Underway
|
Deployed
|
|
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6.0 |
|
3.20 |
|
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|
80 |
42 |
37 |
|
130 |
|
55 |
50 |
|
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|
16 |
|
| |
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)
|
| |
Steadicopter
|
Helivision
|
Underway |
|
|
Small Rotary wing UAV |
|
Vertical take-off. |
Vertical landing. Parechute for emergency. |
|
|
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|
1.50/2.00 |
|
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|
9 / 14 |
30 |
|
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|
10,000 |
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| |
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| |
Silver Arrow
|
Colibri
|
Underway |
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|
Piston |
|
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|
79 |
|
|
13.2 |
22 |
|
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|
6,600 |
|
27 |
1.0 |
|
|
Darter
|
Underway |
|
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|
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|
|
Rotary |
|
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|
|
220 |
|
|
14.0 |
22 |
|
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|
20,000 |
|
50 |
4.0 |
|
|
Hermes 450
|
Complete
|
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Hermes 450S
|
Complete |
Underway |
Limited |
|
|
|
|
|
|
|
Rotary |
|
|
|
|
|
|
|
|
992 |
|
|
34.4 |
220 |
|
|
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|
20,000 |
|
108 |
20.0 |
|
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|
|
Hermes 1500
|
Underway |
|
|
|
|
|
|
|
|
|
Piston |
|
|
|
|
|
|
|
|
3,300 |
|
|
32.8 |
500 |
|
|
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|
30,000 |
|
108 |
36.0 |
|
| |
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Micro-Vee
|
Complete |
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Piston |
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|
100 |
|
|
11.8 |
18 |
|
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|
15,000 |
|
27 |
5.0 |
|
 |
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Sniper
|
Complete |
|
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|
Rotary |
|
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|
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|
375 |
|
|
13.8 |
55 |
|
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|
15,000 |
|
27 |
6.0 |
|
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