LX-WP-40B Turbojet Engine

Experience breakthrough performance with the Telefly LX-WP-40B Turbojet Engine, an exceptional propulsion solution that redefines reliability and efficiency in compact turbojet technology. Manufactured by Telefly - a globally recognized leader in aerospace innovation - this cutting-edge 400N-thrust engine represents the perfect synthesis of advanced engineering and practical functionality. As leading China suppliers specializing in high-performance propulsion systems, we offer exceptional wholesale opportunities for the LX-WP-40B, enabling you to buy discount without compromising on quality or technological sophistication. Request our competitive pricelist today and discover why aerospace professionals worldwide trust Telefly for their critical propulsion needs, all backed by our comprehensive years warranty and global technical support network.

Revolutionary Engineering Excellence

The Telefly LX-WP-40B incorporates groundbreaking technological innovations that establish new benchmarks in compact propulsion. Featuring an advanced single-stage centrifugal compressor with optimized aerofoil geometry paired with a high-efficiency axial flow turbine, this powerplant delivers exceptional thrust-to-weight ratio while maintaining industry-leading specific fuel consumption. The revolutionary annular combustion chamber utilizes precision laser-drilled fuel injectors and advanced swirl stabilization technology, ensuring complete fuel combustion and stable operation across the entire flight envelope. Constructed from titanium alloys and nickel-based superalloys capable of withstanding temperatures exceeding 950°C, the LX-WP-40B maintains structural integrity under the most extreme operating conditions while providing outstanding durability.

Detailed Technical Specifications

Maximum Thrust: 400 N (89.9 lbf) at sea level standard conditions

Dry Weight: 6.8 kg (14.99 lbs) including all mounting accessories

Specific Fuel Consumption: 1.22 kg/N·h (best-in-class efficiency)

Compressor Type: Advanced single-stage centrifugal with 3D aerofoil design

Turbine Section: Single-stage axial flow with directionally solidified blades

Maximum Operating RPM: 105,000 ±400 rpm with active vibration control

Fuel Compatibility: Jet A, Jet A-1, JP-5, JP-8, and sustainable aviation fuels

Starter System: 24V DC high-torque starter with automatic sequencing

Control System: Integrated FADEC with dual-redundant architecture

Operating Altitude: Certified to 12,000 meters (39,370 feet)

Thermal Operating Range: -54°C to +65°C ambient temperature

Service Life: 600+ hours TBO (Time Between Overhauls)

Throttle Response: 0-100% thrust in 3.5 seconds

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