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Bussard German Unmanned Aerial Vehicle (UAV)

Bussard

Tactical Unmanned Aerial Vehicle (UAV)
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Basic Information
Name
Bussard German Unmanned Aerial Vehicle (UAV)
Designation
Bussard
Alternate Designation
Bussard
Equipment Type
Tactical Unmanned Aerial Vehicle (UAV)
Manufacturer
Avilus
Date of Introduction
2025
Description

The Bussard German Unmanned Aerial Vehicle (UAV) is equipped with a laser rangefinder, illuminator, and target designator, allowing it to identify targets at great distances. When combined with radar-based cueing, it enables precise engagement across various domains and mission types. The system integrates seamlessly with battle management systems (BMS), supports beyond-line-of-sight (BLOS) operations, and provides data transmission for effectors. This Ranger Class drone is designed for intelligence, surveillance, target acquisition, reconnaissance (ISTAR), and close air support (CAS). Built on a certified ultralight aircraft platform, it features military-grade avionics and advanced sensor technology—all developed in Germany. The UAV offers exceptional cost-effectiveness and operational capability to address modern military challenges. It includes an electro-optical and infrared (EO/IR) gimbal equipped with a laser designator, allowing for advanced multi-spectral imaging and targeting capabilities. Its state-of-the-art airborne surveillance system boasts an impressive detection range of up to 370 km, enabling it to monitor vast areas with minimal operational assets. Additionally, the military-grade avionics system ensures reliable guidance, navigation, and flight control even in contested environments. The platform is also suitable for manned to unmanned conversion.

Air & Air Defense Specifications
Engine Turbo-charged piston engine or regenerative, multi-fuel turbine (117 hp)
Max Speed 290.0 km/h
Cruise Speed 170.0 km/h
Range 2500.0 km
Endurance 14.00 hrs
Service Ceiling 7600 m
System
Alternate Designation Bussard
Type Unmanned Aerial Vehicle (UAV)
Manufacturer Avilus
Flight Control Primary and secondary flight control system
Navigation Satellite and inertial navigation
Data Links Multiple LOS and BLOS links
Ground Control Duplex GCS integrated in mobile PECC
Battle Management Integrated for planning and monitoring
Packing Size 20 ft ISO-Container
Radar Payload 65 kg (143 lb)
Optical Payload 53 kg (117 lb)
Self-Protection Payload 24 kg (53 lb)
Total Payload 142 kg (313 lb)
Rescue System Automated ballistic parachute deployment
Take-Off Distance 400 m (1312 ft)
Landing Distance 300 m (984 ft)
Dimensions
Enclosing Diameter 7.8 m (25 ft)
Height INA
Propeller Diameter 1.8 m (5.9 ft)
Maximum Takeoff Weight 800 kg (1764 lb)
Automotive
Engine Name INA
Engine Type Turbo-charged piston engine or regenerative, multi-fuel turbine
Engine Power 117 kW (160 HP)
Fuel Type Piston: unleaded gasoline
turbine: F-35 (Jet-A1), F-44 (JP-5), Diesel, UL91, AVGAS
Propeller Automated variable-pitch propeller for maximum efficiency
Maximum Speed 290 km/h (156 kts)
Cruise Speed 170 km/h (92 kts)
Maximum Range 2,500 km (1350 NM)
Service Ceiling 7,600 m (25000 ft)
Endurance 14 hours
Details
Country of Origin Germany
Category UAVs
Air > UAVs
Filter Label
B
Classification
Domain
Air & Air Defense
Equipment Status
Active
Dimensions
Length
Width
Height
Weight
362.87 kg
Operators (1)
Germany
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