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Tipchak (1K133) Russian Unmanned Aerial Vehicle (UAV)

Tipchak

Tactical Unmanned Aerial Vehicle (UAV)
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Basic Information
Name
Tipchak (1K133) Russian Unmanned Aerial Vehicle (UAV)
Designation
Tipchak
Alternate Designation
Tipchak; 1K133; BLA 9M62 (Russian designation); BLA-05 (Russian UAV designation)
Equipment Type
Tactical Unmanned Aerial Vehicle (UAV)
Manufacturer
Design Deaurau Lutch, Russia; Electronics developed by Vega
Date of Introduction
2008
Description

The Tipchak 1K133 is a tactical reconnaissance system developed to replace the Kulon Stroi-P. The platform for the Tipchak is the Rybinsk-based Luch designed 9M62 (BLA-05). The 9M62 is launched by pneumatic catapult, is powered by a single 12hp Hirth piston engine, has an endurance of up to 4 hours, a maximum take-off weight of 70kg, a top speed of 200km/h, and has an entirely composite structure with a metal frame inside for higher strength and onboard camera protection. A parachute is used for recovery. Primary uses are search, detection, recognition, surface object coordinates determination, area surveillance, and adjustment of fires. The Tipchak system consists of a two-part, vehicle-mounted command post, a UAV transport-launch vehicle, a technical maintenance vehicle, and six 9M62 UAVs. The deployment time in field conditions is 15-20 minutes. The UAVs operate in pairs. Based upon the operations in South Ossetia, the Russian military has complained about the Tipchak's UAVs stating that they are too noisy and those that use rocket-assisted take-off give away their launch site. There is also concern about the quality of the reconnaissance as the images provided by the FMV were not of tactical value. A problem with the friend-or-foe system was also reported by the Russian army (Source: TASS-Defense; published May 02, 2017).

Air & Air Defense Specifications
Crew 2
Engine Piston Engine (13 hp)
Max Speed 200.0 km/h
Range 70.0 km
Endurance 2.00 hrs
Variants
Tipchak-M This is a larger air vehicle with greater range and a 33-lb (15-kg) payload that included a side-looking radar, a color digital camera, and gyrostabilized electro-optic sensor. It did not reach the prototype stage.
System
Alternative Designation Tipchak; 1K133; BLA 9M62 (Russian designation); BLA-05 (Russian UAV designation)
Type Medium Altitude, Short Duration Unmanned Aerial Vehicle (UAV)
Manufacturer Design Deaurau Lutch, Russia; Electronics developed by Vega.
Primary Function Reconnaissance and Target Acquisition. The Tipchak can conduct a real-time search, detection, identification, and plotting at a range of up to 25 mi (40 km) from a ground control station.
Complete System The complete system includes a ground control station (GCS), antenna vehicle, operator vehicle, launch vehicle with catapult, maintenance vehicle and up to six piston-engine air vehicles.
Operating Vehicle The operator vehicle system controls telemetry and image data recording, processing and displaying, digital map binding, identification of objects of interest and plotting interaction with management bodies and information users.
Launch Vehicle The launch vehicle stores, transports, conducts pre-flight preparations and pneumatically launches the UAVs.
Maintenance Vehicle A maintenance vehicle prepares UAV recovery and transportation and provides spare parts.
Ground Crew 2 ea
Launch System Pneumatic catapult
Launch Preparation Time 20 minutes
Recovery System Parachute
Automatic Landing and Takeoff Capability No
Mission Review Time 30 minutes
Operating Temperature -40 deg C to +50 deg C
Location Positioning System GLONASS / NAVSTAR
Day/Night Capable Yes
All Weather Capable Yes
Data Transmit Distance INA
Manned-Unmanned Teaming (MUM-T) Capable No
Number of Hard Points 0 ea
Maximum Payload Capacity 14.5 kg
Electronic/Sensors Payload Signal intelligence, chemical reconnaissance equipment, visible/infrared high-resolution line-scan camera.
Dimensions
Length 2.4 m
Wing Span 3.4 m
Height INA
Weight, Maximum Takeoff 60 kg
Weight, Payload 14.5 kg
Automotive
Engine Name 1 x Porsche Engine
Engine Type Piston engine
Engine Power 13 hp
Maximum Speed 200 km/h
Maximum Range 70 km
Maximum Range, from GCS 350 km
Maximum Altitude 3,000 m
Minimum Altitude INA
Endurance 2 hours
Communications
Radio Digital uplink
Retrans Radio No
Armament and Ammunition
Air to Air Missiles No
Air to Ground Missiles No
MIssile Types NA
Bomb Types NA
Armament Weight Total NA
Targeting Capability Can provide targeting for Iskander missiles at distances up to 350 km.
Fire Control
Fire Control System No
Fire Control Radar No
Laser Rangefinder Yes
Laser Designator Yes
Full-Motion Video Yes
Still Camera Yes
Thermal Imaging Sensors Yes
Electro Optical Pod No
SAR/GMTI INA
SIGINT INA
ELINT INA
Digital Data Link Yes, primarily used to communicate with artillery units for laser-guided targeting. Pairings include the 152mm Krasnopol howitzer shell and the Smerch multiple rocket system.
Protection
Stealth Properties No
Heat Signature Reduction No
Add on Armor No
EW INA
EW Counter Measures / CCM No
Counter Measures (Chaffs/Flares) No
Details
Country of Origin Russia
Category UAVs
Air > UAVs
Filter Label
T
Classification
Domain
Air & Air Defense
Equipment Status
Active
Dimensions
Length
2.4 m
Width
3.4 m
Height
Weight
60 kg
Operators (1)
Russia
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