Deltahawk Defense Engines
Made in the USA

DHK2H120 Engine

H120 Engine by Deltahawk Defense

DHK2H120

2-stroke, super-turbocharged compression-ignition aviation engine

The DeltaHawk DHK2H120 represents a new class of U.S.-built, heavy-fuel (Jet-A, JP-5, JP-8) propulsion systems designed for scalable unmanned operations. Purpose-built for medium-size Group 4 UAS platforms, the 80 to 120 hp class fills a critical gap in long-endurance, medium-power propulsion within the U.S. market. Designed for sustained, efficient operation, it enables extended mission duration, increased payload capability, and reliable performance for reusable unmanned systems. Leveraging a scaled architecture with significant commonality to larger DeltaHawk engines, the DHK2H120 delivers proven performance, simplified integration, and reduced lifecycle cost for advanced unmanned platforms.

  • 2-stroke, super-turbocharged compression-ignition architecture delivering efficient, sustained power output
  • Multi-fuel capability, including Jet-A, JP-5, and JP-8, enabling logistics alignment across military operations
  • Scaled architecture with approximately 80% parts commonality with larger DeltaHawk engines
  • Simplified mechanical design with minimal electronics, increasing reliability and reducing system complexity
  • Optimized for long-endurance missions requiring consistent medium-power output
  • Purpose-built to address the gap in U.S.-produced propulsion for medium-size Group 4 UAS platforms
  • Designed for reusable, long-endurance systems requiring sustained power over extended mission durations
  • Proven architecture derived from larger, high-performance DeltaHawk engine platforms
  • Integration-ready design adaptable to a wide range of Group 4 unmanned aircraft
  • U.S. design and built solution supporting domestic supply chain resilience
  • Power class: 80-120 hp
  • Engine type: 2-cylinder, 2-stroke compression-ignition
  • Fuel compatibility: Jet-A, Jet-A1, JP-5, JP-8, and approved heavy fuels
  • Cooling system: Liquid-cooled
  • Induction: Super-turbocharged architecture
  • Configuration: Modular, scaled design for flexible integration
  • Target applications: Group 4 UAS, long-endurance ISR platforms, reusable unmanned systems, small hybrid-electric systems
  • Compatible with standard aviation heavy fuel infrastructure
  • Designed for integration with medium-size unmanned airframe architectures
  • Minimal support equipment required for operation and deployment
  • Suitable for long-duration missions in distributed and austere environments
  • Scalable manufacturing aligned with production and deployment requirements