Penguin BE UAV

Technical Specification

Product specifications


21.5 kg (47.4 lb)

Empty weight (Excluding payload, with standard landing gear, with battery cartridge)

14.9 kg (32.8 lb)

Wing span

3.3 m (10.8 ft)


2.3 m (7.5 ft)

Wing area

0.79 m² (8.5 sq ft)

Propulsion type

Geared brushless electric motor

Propulsion power

2700 W

Battery type

Lithium polymer

Battery cartridge capacity

640 Wh

Onboard voltage

6 V / 12 V

Onboard continuous power

100 W

Max payload

6.6 kg (14.5 lb)

Takeoff method

Catapult, runway or car top launch

Environmental protection

Sealed against rain and snow


Endurance (in belly landing configuration)

110 minutes with 2.8 kg (6.2 lb) payload

Cruise speed

22 m/s (43 knots)

Stall speed (with high lift system), Sea level altitude, 15 kg (33 lb) aircraft weight, 15 °C

13 m/s (25.3 knots)

Max level speed

36 m/s (70 knots)

Takeoff run, Sea level altitude, 15 kg (33 lb) aircraft weight, 15 °C, concrete runway

30 m (98 ft)

CL max (45o flap deflection)


CL max (clean wing)



6000 m (19 685 ft) AMSL

Universal Payload Mount

Electric Penguin B has a swappable universal payload mount that can be removed in seconds and used for various payloads. Payload mount is inserted from the underneath of the fuselage and includes a large section of the lower fuselage surface to facilitate the installation of the camera gimbal or other payload. The most sophisticated payloads such as retractable gimbals can be installed by integrators into the fuselage and utilize the available space efficiently. The universal payload mount has predetermined mounting points that are precisely machined into the aluminium frame as well as removable ballast slugs that will simplify the payload integration process considerably. Due to the compact size of electric propulsion and battery cartridge, there is a large amount of space available for payload integrators. The fuselage is split into two main payload areas – the forward payload bay and the rear payload bay.

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