The constant temperature test chamber is a testing device that simulates high-temperature, low-temperature, and wet heat environments. It is widely used in electronics, aviation, scientific research, and other fields. Its core function is to evaluate the endurance of products through precise temperature and humidity control.
Technical Specifications
Capacity: 100 to 12,000L
Temperature Range: -70°C to +180°C
Temperature Change Rate: 5°C/min to 25°C/min (optional)
Temperature Fluctuation: < ±0.5°C
Temperature Deviation: < ±2.0°C
Temperature Uniformity: < 2.0°C
Patent No.: CN201920954255.X
Features:
1.Cold/Hot Balance Technology
Ensures extreme temperature stability while reducing energy consumption by 30%.
2.Smart Control System (v3.0)
Provides real-time monitoring and traceability of operational status, eliminating manual checks and significantly cutting labor and maintenance costs.
3.High-Speed Transition
Achieves rapid temperature shifts with mechanical refrigeration, ensuring reliability and precision for critical testing environments.
4.User-Centric Design
Customizable chamber sizes and intuitive controls meet diverse industry needs, from aerospace to electronics validation.
TESTEQ Rapid Temperature Change Test Chamber ― Standards Compliance & Testing Capabilities
Fully Compliant with Major International Test Standards
The TESTEQ Rapid Temperature Change Test Chamber is engineered to meet and exceed the stringent requirements of key industry standards, including:
JEDEC Standard JESD22-A104G
(Temperature Cycling)
― Reliably performs high-speed temperature cycling tests for semiconductor and electronic components to evaluate their robustness against thermal fatigue and interconnect failures.
MIL-STD
(Military Standard Environmental Test Methods)
― Supports a wide range of defense and aerospace environmental stress screening (ESS) tests, including rapid transition thermal cycling as required by MIL-STD-810 and MIL-STD-883.
RTCA/DO-160
(Environmental Conditions and Test Procedures for Airborne Equipment)
― Ideal for validating avionics equipment under extreme temperature variations and rapid transition conditions per Sections 4.0 and 5.0.