LH-04

Native Parallel Hybrid™ Propulsion,Built for the Mission

Designed for fixed-wing & VTOL

MTOW60-120KG132-265 LB
Electrical power9,135W12.25 HP
Cruise power (ICE)5,960W8.00 HP
Unit weight6.1KG13.44 LB

Overview

Hybrid From the Ground Up. LH-04 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 60-120 KG / 132-265 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

12-20 hrs Endurance on ICE
15-25 min Silent Flight on electric power
600 W In-Flight Battery Charging for continuous avionics and sensor power

For typical 60-120 KG MTOW fixed-wing platforms

Operational Specifications

Usage	Hybrid propulsion system for fixed-wing/VTOL
Typical MTOW	60-120 KG / 132-265 LB
UAS Group (US DoD)	Group 3
Max electric output power	9,135 W / 12.25 HP
Nominal electric power output (avionics/charging)	600 W
Max gasoline output power	5,960 W / 8.00 HP
Engine type	Air-cooled, 2-stroke Boxer cylinder configuration
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 - 0.58-0.61 KG/kW·H
Full system weight	6.1 KG / 13.44 LB
Operating temperature	-20°C to +50°C / -4°F to +122°F
Operating altitude	0-5,480 M / 0-18,000 FT
MTBO	250 hours
Recommended propeller	28" - 34"