This 200 kg thrust turbojet engine is used in aircraft such as drones, target dr
Technical Specifications for 6.4kg Micro Turbojet Engine Thrust：6.4kg / 64N / 1
The Mach number range of the transonic wind tunnel test is roughly 0.8~1.4, and
Size parameters: Launch preparation time: 15min Working temperature: -30°～+50° L
Nm-80wp turbojet engine is a turbojet engine composed of a single stage centrifu
The air propeller is a tool that converts the power of the aero engine into the
The NM-150P turbojet engine is a small turbojet engine composed of a single-stag
The icing wind tunnel is a large-scale special wind tunnel with complex performa
Product introduction and use This antenna has BD-2 B3/B1/S, GPS-L1 signal
600kW military drone heavy fuel engine Main product features： Boxer 8 cylinders
Product parameters: Type: Fixed Pitch Rally Propeller Propeller diameter: 3m Pro
Product overview SNC100C-DGI integrated navigation system is composed of MEMS se
Product overview SNC100C-LITE integrated navigation system has built-in high-per
1. Product overview SNC200A-E inertial navigation system has built-in high-perf
Product overview SNC300A-DGI is based on cost-effective closed-loop fiber optic
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Product overview SNC300D-DGI is based on cost-effective closed-loop fiber optic
Custom aircraft engine company was established in 1951 and has more than 70 year
CPU GPU Liquid Cold Plate Features 1. High thermal conductivity: Efficiently tra
A solar fuse is a special purpose fuse used in photovoltaic (PV) or solar power
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