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Penguin C Mk2 MIL UAS

TECHNICAL SPECIFICATION

Aircraft Specifications

Wingspan 3.3 m / 10.8 ft
MTOW Group 2: 25 kg / 55 lb

Group 3: 28 kg / 62 lb

Endurance 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

Range 180 km / 112 miles
Cruise speed 47-49 knots
Max level speed 62.2 knots
Ceiling 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
Navigation 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

Detectability Not detectable at 1 km / 0.62 miles
Transponder 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
Frequency UHF, L, C, or S band; customizable
Link Rate Up to 20 Mbps
Output power Up to 10 W
Encryption AES 256

System Specifications

Autopilot 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
Landing Computer assisted parachute recovery; airbag
Crew size 2
Preparation time Less than 1 hour from pallet to launch ready
Mobility 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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