Orlan-10 Russian Unmanned Aerial Vehicle (UAV)
STC Orlan-10
Multirole Fighter Aircraft
Other
Basic Information
Name
Orlan-10 Russian Unmanned Aerial Vehicle (UAV)
Designation
STC Orlan-10
Alternate Designation
STC Orlan-10
Equipment Type
Multirole Fighter Aircraft
Manufacturer
Special Technology Center LLC
Date of Introduction
2010
Description
Orlan-10 is a medium-range, multi-purpose unmanned aerial vehicle (UAV) developed by Russian firm Special Technology Center LLC in St Petersburg. The UAV is in service with the Ministry of Defense of the Russian Federation. It is intended for a variety of missions including aerial reconnaissance, observation, monitoring, search and rescue, combat training, jamming, detection of radio signals, and target tracking. The drone is usually used in a group of two or three, where the first one is used for reconnaissance in a height of 1-1.5 km, the second one for electronic warfare and the third one as a transponder that transmits intelligence information to the control center
Air & Air Defense Specifications
Engine
Gasoline
Max Speed
150.0 km/h
Range
150.0 km
Endurance
16.00 hrs
System
Alternative Designation
STC Orlan-10
Type
Medium-range, multi-purpose unmanned aerial vehicle (UAV)
Manufacturer
Special Technology Center LLC
Primary Function
The Orlan-10 is intended for a variety of missions including aerial reconnaissance, observation, monitoring, search and rescue, combat training, jamming, detection of radio signals, and target tracking.
Cost
US $87,000 and US $120,000
Day/Night Capable
Yes
All Weather Capable
Yes
Ground Crew
MP32M1 command and control vehicle. The ground segment can control up to four aerial vehicles simultaneously.
Autopilot Capabile
Yes, operates autonomously based on pre-defined waypoints
Command and Control Modes
Both autonomous and remote control modes
Location Positioning System
Yes
Manned-Unmanned Teaming (MUM-T) Capable
No
Automatic Landing and Takeoff Capability
No
Transmit Telemetry Data Range
120 km and 600 km from the launch station
Launch System
Folding catapult
Recovery System
Via Parachute Recovery
Note
The Orlan-10 complex consists of unmanned aerial vehicles, launch and recovery systems, ground control segment, and swappable payloads.
Dimensions
Length (Fuselage)
2.0 m
Width (Wing Span)
3.1 m
Height
INA
Weight, Empty
12.5 kg
Weight, Maximum Takeoff
16.5 kg
Note
The UAV’s modular design is provided with a number of interchangeable payloads allowing for greater mission flexibility.
Automotive
Engine Name
1 x A-95 Engine
Engine Type
Gasoline-Fueled Engine
Number of Blades
2 ea
Engine Power
INA
Cruising Range
150 km
Speed, Maximum
150 km/h
Speed, Cruising
110 km/h
Ceiling
5,000 m
Endurance
16 hours
Maximum Wind Speed at the Start
10 m/s
Operating Temperatures
−30 to +40 °C
Fire Control
Laser Rangefinder
INA
Day Light Camera
Yes
Video Camera
Yes
Gyro Stabilized Camera Pod
Yes
Thermal Imaging Sensors
Yes
Thermal Imaging Camera
Yes
Real-time Intelligence Capable
Yes
3D Maps
Yes
Note
The imagery, video and other sensor data collected by the payloads is transmitted to the ground control station in real-time, through a data link.
Protection
Stealth Properties
No
Heat Signature Reduction
INA
Add on Armor
No
EW
Equipment Available
EW Counter Measures / CCM
Equipment Available
Counter Measures (Chaffs/Flares)
INA
Details
Country of Origin
Russia
Category
UAVs
Air > UAVs
Filter Label
O
Classification
Domain
Air & Air Defense
Equipment Status
Active
Dimensions
Length
2 m
Width
3.1 m
Height
—
Weight
16.5 kg
Operators (5)
Russia
Ukraine
Belarus
Myanmar
Syria
Something went wrong. Please reload the page.
Reload