Penguin C Mk2 MIL UAS

Technical Specification

Aircraft Specifications


3.3 m / 10.8 ft


Group 2: 25 kg / 55 lb

Group 3: 28 kg / 62 lb


Group 2: 25.5 hours w/Epsilon 140LC and 17.5 hours w/Epsilon 180

Group 3: 25.5 hours w/Epsilon 140LC and 22 hours w/Epsilon 180


180 km / 112 miles

Cruise speed

47-49 knots

Max level speed

62.2 knots


5,000 m / 16,400 ft MSL

Max takeoff altitude

3,048 m / 10,000 ft AMSL

Operational t°

-30°C to 50°C / -22°F to +122°F


GPS and magnetometer (for GPS-denied environments)

Anti-icing measures

Heated Pitot tube

Weather limitations

Rain < 5 mm/ hour / 0.2 inches/hour

20 knot sustained winds


Not detectable at 1 km / 0.62 miles


Mode 5 Mark XIIB or ADS-B

Propulsion System

Engine type

28cc EFI module; proprietary low noise mufler

Temperature control system

Automatically controlled via mechanical flap

Fuel type

Unleaded gasoline or C10

Generator system

150 W onboard generator system

Data Link Specifications

Datalink manufacturer

Silvus MIMO with Mesh


UHF, L, C, or S band; customizable

Link Rate

Up to 20 Mbps

Output power

Up to 10 W


AES 256

System Specifications


Piccolo, Cloud Cap Technology

Ground Control Station

Portable, Dual touchscreen displays

Tracking antenna

Tracking high gain directional and omnidirectional antenna

Take off

Fully autonomous pneumatic catapult with 12 kJ launch energy


Computer assisted parachute recovery; airbag

Crew size


Preparation time

Less than 1 hour from pallet to launch ready


System fits in 6 or fewer cases,

weight < 450 kg / 1,000 lb

Gimbal Options

Gimbal Comparison

System Footprint

3 Aircraft, 1 launcher, 1 Tracking Antenna, 1 Ground Control Station

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