LH-01

Native Parallel Hybrid™ Propulsion,Built for the Mission

Designed for fixed-wing & VTOL

MTOW15-30KG33-66 LB
Electrical power2,755W3.69 HP
Cruise power (ICE)1,415W1.9 HP
Unit weight2.5KG5.5 LB

Overview

Hybrid From the Ground Up. LH-01 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 15-30 KG / 33-66 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

8-12 hrs Endurance on ICE
30-45 min Silent Flight on electric power
150 W In-Flight Battery Charging for continuous avionics and sensor power

For typical 15-30 KG MTOW fixed-wing platforms

Operational Specifications

Usage	Hybrid propulsion system for fixed-wing/VTOL
Typical MTOW	15-30 KG / 33-66 LB
UAS Group (US DoD)	Group 2-3
Max electric output power	2,755 W / 3.69 HP
Nominal electric power output (avionics/charging)	150 W
Max gasoline output power	1,415 W / 1.9 HP
Engine type	Air-cooled, 2-stroke single cylinder
Starting method	Automatic
Fuel type	Pre Mixed Gasoline / Heavy fuel + 4% Two Stroke Oil
Fuel delivery	EFI (Electronic Fuel Injection)
Average nominal specific fuel consumption rate	Gasoline - 0.47-0.52 KG/kW·HHeavy Fuel - 0.50-0.55 KG/kW·H
Full system weight	2.5 KG / 5.5 LB
Operating temperature	-20°C to +50°C / -4°F to +122°F
Operating altitude	0-3,040 M / 0-10,000 FT
MTBO	250 hours
Recommended propeller	16" - 20"