LH-03

Native Parallel Hybrid™ Propulsion,Built for the Mission

Designed for fixed-wing & VTOL

MTOW50-80KG110-176 LB
Electrical power7,355W9.86 HP
Cruise power (ICE)3,400W4.55 HP
Unit weight4.65KG10.25 LB

Overview

Hybrid From the Ground Up. LH-03 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 50-80 KG / 110-176 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

10-16 hrs Endurance on ICE
20-30 min Silent Flight on electric power
400 W In-Flight Battery Charging for continuous avionics and sensor power

For typical 50-80 KG MTOW fixed-wing platforms

Operational Specifications

Usage	Hybrid propulsion system for fixed-wing/VTOL
Typical MTOW	50-80 KG / 110-176 LB
UAS Group (US DoD)	Group 3
Max electric output power	7,355 W / 9.86 HP
Nominal electric power output (avionics/charging)	400 W
Max gasoline output power	3,400 W / 4.55 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 - 0.56-0.6 KG/kW·H
Full system weight	4.65 KG / 10.25 LB
Operating temperature	-20°C to +50°C / -4°F to +122°F
Operating altitude	0-4,870 M / 0-16,000 FT
MTBO	250 hours
Recommended propeller	24" - 28"