By accurately controlling the internal pressure of the cabin, the space working environment of the spacecraft is simulated. Monitor the pressure difference inside and outside the cabin in real time to ensure that the pressure change range is ≤0.5%FS.
Equipped with HX-2000 series data acquisition module, including:
Typical test parameters:
Project | Standard value | Allowable deviation |
---|---|---|
Test pressure | 1.5 times working pressure | ±0.5%FS |
Stabilization time | ≥30min | +5/-0min |
Test Medium | Helium-nitrogen mixture (He 10% + N₂ 90%) |
---|---|
Test Pressure | 1.2 times working pressure (Max 8bar) |
Rate of Pressure Increase | ≤0.5bar/s |
Utilize a helium mass spectrometer to detect helium leaks, suitable for high-precision leak detection.
Detect small leak points by measuring changes in small gas flow.
Connect the part to the testing equipment, slowly inflate it with the test gas (such as helium), and gradually pressurize it to the predetermined value.
During the pressurization process, use high-sensitivity sensors to monitor the surface of the part and detect any leak points.
Record real-time parameters such as pressure, temperature, and leak rate during the testing process. Analyze the data to evaluate the air tightness of the part.