Why choose Bulldog 2000?
Twin-rotor architecture, designed for heavy-lift missions. Enhanced stability and efficient transport performance in demanding operational environments.
Twin-rotor architecture, designed for heavy-lift missions. Enhanced stability and efficient transport performance in demanding operational environments.
Heavy Payload Capacity
Lift up to 40 kg without compromise
Higher Transit Speed
Over 100 km/h for rapid missions
Wind & Weather Stability
Consistent control in challenging conditionst
Technical Overview
Key Characteristics
Key Characteristics
Key Characteristics
Dimensions (L x W x H)
2780 x 580 x 628 mm
Dimensions (L x W x H)
2780 x 580 x 628 mm
Rotor Diameter
2 x 2254 mm
Rotor Diameter
2 x 2254 mm
Max. Take-off Weight
80 Kg
Max. Take-off Weight
80 Kg
Weight (w\o batteries)
28 Kg
Weight (w\o batteries)
28 Kg
Payload Capacity
Up to 40 Kg
Payload Capacity
Up to 40 Kg
Endurance
70 min.
Endurance
70 min.
Optimal Cruise Speed
19 m/s (36,9 kn)
Optimal Cruise Speed
19 m/s (36,9 kn)
Max. Horizontal Speed
33 m/s (64.1 kn)
Max. Horizontal Speed
33 m/s (64.1 kn)
Max. Climb & Descent Speed
3 m/s
Max. Climb & Descent Speed
3 m/s
Deployment Area
18 m²
Deployment Area
18 m²
Deployment Time
<10 min.
Deployment Time
<10 min.
Enviromental
Enviromental
Enviromental
Wind Resistance
20 m/s (38.9 kn)
Wind Resistance
20 m/s (38.9 kn)
Operating Temperature
-20° to +50° C (-4° to +122° F)
Operating Temperature
-20° to +50° C (-4° to +122° F)
Max. Flight Altitude
4000 m
Max. Flight Altitude
4000 m
IP Rating
IP54
IP Rating
IP54
Engineered for demanding missions.
Built for missions where reliability defines success.
Engineered for demanding missions.
Built for missions where reliability defines success.
Engineered for demanding missions.
Built for missions where reliability defines success.