Penguin C UAS

Technical Specification

Aircraft Specifications

Wingspan

3.3 m / 10.8 ft

MTOW

23 kg / 50.7 lbs

Endurance

< 20 hours depending on payload

Range

100 km / 60 miles

Cruise speed

19-22 m/s / 37-43 knots

Max level speed

32 m/s / 62.2 knots

Ceiling

5000 m / 16 400 ft AMSL

Takeoff

Pneumatic Catapult, fully autonomous

Maximum takeoff altitude

3000 m / 10 000 ft AMSL

Recovery

Parachute recovery, airbag

Operational temperature

-40 °C to +50 °C depending on configuration

Anti-icing measures

Heated Pitot-static tube. Continuous flight operations in icing conditions are not approved.

Environmental protection

< 5 mm/h rain. Pitot with drain.

Propulsion System

Engine type

Fuel injected, single cylinder, two-stroke internal combustion engine

Temperature control system

Automatically controlled via mechanical flap

Fuel type

Unleaded 98 octane (RON) gasoline, oil mix

Generator system

100 W or 150 W onboard generator system depending on configuration

Payload Specifications

Payload type

Day/night gyro stabilized Epsilon range of payloads

Advanced features

Target Tracking, Electronic Stabilization, Moving Target Indicator

Mounting

Motorized retract with anti-vibration damping

Data Link Specifications

Frequency

2.304–2.390 GHz

2.402-2.482 GHz

2.500-2.570 GHz

5.000-5.900 GHz

Link rate

Up to 12 Mbps

Encryption

128 bit AES

256 bit AES

Flight Control System

Autopilot type

Piccolo, Cloud Cap Technology

Ground Control Station

Type

Portable, dual touchscreen displays

Ground Data Terminal

Type

Tracking high gain directional antenna

Catapult System

Type

Portable pneumatic, 6000 J launch energy

Dimensions

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