Purpose:

1. Equipment for simulating the space environment. Used to test the spacecraft's resistance to vacuum, cold black, solar radiation, magnetic fields, and its ability to withstand high-energy particle radiation, solar wind, and micro-meteoroids.

2. Thermal vacuum environment simulator. Used to simulate the three basic parameters of space: vacuum, cold black, and solar radiation, for conducting thermal vacuum tests and thermal balance tests of spacecraft.

3. Space dynamics simulator. A large-scale low-vacuum simulation system.

4. Space combined environment simulator. The simulated environment includes solar radiation, ultraviolet rays, electrons, protons, solar wind, extreme high vacuum, thermal cycling, plasma, etc., used for the research and testing of spacecraft components and materials.

Technical Parameters:

Main chamber diameter: Customized according to customer requirements

Main chamber total length: Customized according to customer requirements

Minimum temperature: Approximately -190°C (Space temperature: Approximately -270°C)

Minimum vacuum level: 1/1,000,000 Pascal (Space vacuum level: 1/10,000,000 Pascal)

Maximum radiation intensity: Approximately 1.8 kW/m2