LH-02

Native Parallel Hybrid™ Propulsion,Built for the Mission

Designed for fixed-wing & VTOL

MTOW25-45KG55-99 LB
Electrical power3,600W4.82 HP
Cruise power (ICE)2,385W3.2 HP
Unit weight3.3KG7.3 LB

Overview

Hybrid From the Ground Up. LH-02 is a next-generation propulsion system engineered with our proprietary Native Parallel Hybrid™ architecture from day one. Designed for tactical UAVs and loitering munitions in the 25-45 KG / 55-99 LB MTOW class, it combines endurance, flexibility, and assurance in one compact, mission-ready system.

Built for What Missions Demand. Up to 5× longer endurance, silent operation when required, and field-proven reliability. Seamless switching between electric and combustion modes, in-flight battery charging, and built-in redundancy keep the mission going.

Key Capabilities

10-12 hrs Endurance on ICE
25-40 min Silent Flight on electric power
250 W In-Flight Battery Charging for continuous avionics and sensor power

For typical 25-45 KG MTOW fixed-wing platforms

Operational Specifications

Usage	Hybrid propulsion system for fixed-wing/VTOL
Typical MTOW	25-45 KG / 55-99 LB
UAS Group (US DoD)	Group 2-3
Max electric output power	3,600 W / 4.82 HP
Nominal electric power output (avionics/charging)	250 W
Max gasoline output power	2,385 W / 3.2 HP
Engine type	Air-cooled, 2-stroke single cylinder
Starting method	Automatic
Fuel type	Pre Mixed Gasoline + 4% Two Stroke Oil
Fuel delivery	EFI (Electronic Fuel Injection)
Average nominal specific fuel consumption rate	Gasoline - 0.43-0.48 KG/kW·H
Full system weight	3.3 KG / 7.3 LB
Operating temperature	-20°C to +50°C / -4°F to +122°F
Operating altitude	0-3,960 M / 0-13,000 FT
MTBO	250 hours
Recommended propeller	20" - 24"