Variable power system

Variable power system is a propulsion system that can adjust its performance according to flight conditions or mission requirements. The core feature of this system is its "variability", which means it can change the thrust size, thrust direction, or working mode to adapt to different flight stages or mission requirements. The variable power system is the key to the successful soft landing of the probe on the moon.

The unit is designed for unsupervised public use: controls are recessed or shielded, moving parts are enclosed, and the interface is operable by a child of about six with no instruction. Where a screen is used, the language can be switched without changing the hardware, and the content can be replaced on site.

7500N Variable Thrust Engine: A Variable Thrust Engine is an engine that can adjust thrust output and provide different thrust under different operating conditions as needed. This type of engine is commonly used in aircraft, such as airplanes and rockets. Variable thrust engines typically have multiple thrust adjustment modes, including the following three: staged thrust adjustment; Nozzle adjustment; Hybrid cycle engine. The advantage of a variable thrust engine is that it can adjust thrust according to demand, improving the performance and efficiency of the aircraft. It can adapt to different task requirements, reduce fuel consumption, and provide greater flexibility and maneuverability. However, at the same time, the design and control of variable thrust engines are complex, costly, and require corresponding technical support for maintenance and operation. Therefore, in practical applications, it is necessary to comprehensively consider both cost and performance.