Penguin B UAV

Technical Specification

Product specifications

MTOW

21.5 kg (47.4 lb)

Empty weight (Penguin B with engine and servo package, excl. fuel and payload)

11.5 kg (25.4 lb)

Wing span

3.3 m (10.8 ft)

Length

2.3 m (7.5 ft)

Wing area

0.79 m² (8.5 sq ft)

Powerplant

2.5 hp

Max payload

10 kg (22 lb)

Takeoff method

Catapult, runway or car-top launch

Environmental protection

Sealed against rain and snow

Performance

Endurance (Penguin B with fuel injected engine and 7.5 liter fuel tank, depends on payload)

20+ hours

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)

1.7

CL max (clean wing)

1.3

Universal Payload Mount

Penguin B has a swappable universal payload mount that can be removed in seconds and used for various payloads. 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 in the aluminum frame as well as removable ballast slugs that will simplify the payload integration process considerably.

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