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HJP100 Micro-Turbojet Engine
The HJP100 is a high-performance, lightweight micro-turbojet engine designed for small unmanned aerial vehicles (UAVs), experimental aircraft, and other aviation applications requiring compact propulsion. It delivers impressive thrust and environmental adaptability within a highly constrained size and weight profile.
Core Performance Features:
Substantial Thrust: Delivers a maximum thrust of98 kgf (approximately 961 N), providing ample power for small aircraft.
Exceptional Lightweight: Engine dry weight is only 14.2 kg, offering an excellent thrust-to-weight ratio and significantly reducing the overall weight burden on the airframe.
Compact Design:Features extremely compact dimensions with a maximum length of 690 mm and maximum diameter of 202 mm, facilitating easy installation and integration into space-constrained aircraft.
High-Speed Operation:Capable of reaching a maximum rotational speed of 65,000 rpm, reflecting its efficient aerodynamic and mechanical design.
Broad Environmental Adaptability:
High Altitude Capability:Operates effectively at altitudes up to8,000 meters, meeting requirements for high-altitude or plateau flight.
Wide Temperature Range:Functions reliably across a broad ambient temperature range from-40°C to +45°C, demonstrating good cold-start and hot-weather operational capability.
High-Speed Flight:Supports aircraft achieving a maximum flight speed ofMach 0.8.
Fuel Efficiency:Features a fuel consumption rate of1.45 kg/(kgf·h), which is typical for micro-turbojet engines, balancing performance with endurance needs.
Thermal Management:Maximum Exhaust Gas Temperature (EGT) is controlled at750°C, ensuring reliability and longevity of core components under high-temperature conditions.
Application Areas:
Leveraging its light weight, high thrust, and robust environmental adaptability, the HJP100 is ideally suited for:
Medium-to-large fixed-wing/delta-wing UAVs
Manned/Unmanned experimental small aircraft
High-speed radio-controlled model aircraft (advanced applications)
Research platforms requiring small-scale jet propulsion
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