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KUB-2E Russian Unmanned Aerial Vehicle (UAV)

KUB-2-2E

Tactical Unmanned Aerial Vehicle (UAV)
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Basic Information
Name
KUB-2E Russian Unmanned Aerial Vehicle (UAV)
Designation
KUB-2-2E
Alternate Designation
KUB-2-2E
Equipment Type
Tactical Unmanned Aerial Vehicle (UAV)
Manufacturer
Kalashnikov Concern
Date of Introduction
2025
Description

The KUB-2E Russian Unmanned Aerial Vehicle (UAV) reflects maturation of Russian loitering munition doctrine and represents credible fielding of medium-class precision strike capability within a contested air defense environment. Technical specifications—40+ kilometer range, GPS-independent guidance, day/night targeting, multi-mode warhead capability—position the system as operationally relevant tool for tactical commanders requiring responsive precision fires without exposed platform risk. The catapult launch architecture, simplified compared to vehicle-integrated systems, enables dispersed employment by smaller units and supports rapid relocation-to-minimize counter-battery exposure, aligning with modern force protection doctrine.

Air & Air Defense Specifications
Engine The propulsion architecture utilizes a rear-mounted electric motor powering a two-blade pushing propeller, with battery placement optimized at the center of gravity to maximize flight efficiency.
Max Speed 150.0 km/h
Cruise Speed 120.0 km/h
Range 40.0 km
Endurance 25.00 hrs
Service Ceiling 2000 m
Payload Capacity 4 kg
Variants
KUB-2-1E The small-class KUB-2-1E, at 12 kilograms take-off mass with a 3.9-kilogram thermobaric warhead, delivers precision strikes against individual personnel and unarmored equipment over 20+ kilometer ranges with sustained flight times exceeding 20 minutes.
System
Alternate Designation KUB-2-2E
Type Unmanned Aerial Vehicle (UAV)
Manufacturer Kalashnikov
Payload Capacity 4.6 kg
Warhead Type Thermobaric
Guidance System Primary guidance utilizes Global Navigation Satellite System (GNSS) coordinates for pre-programmed waypoint navigation, enabling operator-planned engagement profiles against static or predictable targets. Critically, the system integrates GPS-independent electro-optical and automatic optoelectronic guidance modes, employing day/night thermal imaging and artificial intelligence-assisted target recognition to track moving objectives and engage time-sensitive targets even when satellite navigation is degraded or denied.
Operator Control Operator control extends from a mobile unified command station managing mission planning, launch sequencing, target observation, and strike authorization through real-time video and telemetry relay systems. The three-person crew structure—separation of mission planning, launch control, and target assessment functions—reflects mature operational doctrine developed through intensive field deployment. This architecture enables rapid reaction to emerging targets while maintaining precise strike accountability and minimizing collateral engagement risk through operator confirmation of target identity and position before final dive sequence initiation.
Integration Capability The integration capability with the Skat-350M reconnaissance drone creates a tandem reconnaissance-strike system, enabling forward reconnaissance elements to detect, identify, and coordinate target handoff to loitering munition operators, significantly extending target acquisition range and reducing time-to-strike latency compared to autonomous prosecution.
Dimensions
Length INA
Height INA
Wingspan INA
Maximum Takeoff Weight 14.5 kg
Automotive
Engine Name INA
Engine Type The propulsion architecture utilizes a rear-mounted electric motor powering a two-blade pushing propeller, with battery placement optimized at the center of gravity to maximize flight efficiency.
Engine Power INA
Maximum Speed 150 km/h
Cruise Speed 120 km/h
Maximum Range 40 km
Service Ceiling 2,000 m
Endurance 25 min
Details
Country of Origin Russia
Category UAVs
Air > UAVs
Filter Label
K
Classification
Domain
Air & Air Defense
Equipment Status
Active
Dimensions
Length
Width
Height
Weight
14.5 kg
Operators (1)
Russia
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