HJP40 Turbofan Engine

HJP40 Turbofan Engine – Lightweight Powerhouse, Setting a New Benchmark for Performance

Designed for High-Performance UAVs,  Aircraft

Core Advantages

• Extreme Thrust-to-Weight Ratio: Merely 4.5 kg dry weight, delivering 45 kgf max thrust. A thrust-to-weight ratio exceeding 10:1 provides potent kinetic energy for high-speed aircraft.

• Ultra-Compact Design: Max diameter 160mm, length 410mm. Its lightweight, compact form integrates seamlessly into various small flight platforms, unlocking space potential.

• Full Environmental Adaptability: Operational temperature range from -40°C to 45°C, suitable for altitudes up to 7000m ASL. Undaunted by extreme cold, heat, or high-altitude challenges.

• Efficient & Reliable Operation: Fuel consumption as low as 1.45kg/(kgf·h), combined with a controllable exhaust temperature of 750°C, ensures prolonged stable output.

Peak Performance

• 82,000 RPM Ultra-High Rotational Speed

• 0.7 Ma High-Speed Flight Capability

• Rapid Response, Power On-Demand

Why Choose the HJP40?

"A powerhouse in the palm of your hand, redefining the performance boundaries of lightweight flight."

– Engineered for cutting-edge aircraft demanding speed, efficiency, and reliability. Empowering clients to seize the technological high ground in the micro-propulsion domain.