Aircraft and satellite components operate in some of the most
extreme and demanding environments known to man. From the frigid
temperatures of high - altitude flight to the intense heat and
variable humidity in space, these components must be able to
withstand a wide range of conditions to ensure the safety and
success of their missions. Our high - precision temperature
humidity test chamber is specifically designed to meet the rigorous
testing requirements of aircraft and satellite component
manufacturers. This advanced chamber provides a controlled
environment where components can be tested under precisely
simulated conditions, allowing for the evaluation of their
performance, reliability, and durability.
The core strength of this test chamber lies in its ability to
achieve ultra - high precision in temperature and humidity control.
The temperature can be adjusted within an extensive range,
typically from - 70°C to 150°C, with an astonishing precision of
±0.1°C. Humidity levels can be precisely regulated from 5% to 98%
relative humidity (RH), with a precision of ±2% RH. This level of
accuracy is crucial for mimicking the exact environmental
conditions that aircraft and satellite components will encounter
during their operational lifetimes. Whether it's the extreme cold
of space or the high - humidity conditions during a tropical
flight, the chamber can replicate these scenarios with unparalleled
precision.
To accommodate the diverse testing needs of aircraft and satellite
components, the chamber offers a wide variety of customizable test
profiles. Users can create complex, multi - stage test sequences
that simulate the actual environmental changes a component will
experience during its mission. For example, a test profile could
include rapid temperature changes to mimic the transition from a
hot launch environment to the cold of space, or cyclic humidity
variations to simulate the effects of different atmospheric
conditions. These custom - programmed test scenarios allow for a
more comprehensive evaluation of component performance under
realistic conditions.
In addition to temperature and humidity control, the test chamber
is equipped with advanced vacuum and pressure control systems. This
feature is essential for simulating the low - pressure and vacuum
conditions that satellite components encounter in space. The
chamber can achieve extremely low pressures, down to [X] Pascal,
allowing for the testing of components' ability to function in a
near - vacuum environment. Similarly, it can also simulate high -
pressure conditions, such as those experienced during aircraft
takeoff and landing, to ensure the components' structural integrity
and performance under stress.
Aircraft and satellite components often experience rapid changes in
temperature and humidity during their operation. To accurately test
their ability to adapt to these changes, the test chamber is
capable of achieving high - speed temperature and humidity
transitions. The temperature can change at a rate of up to [X] °C
per minute, and the humidity can be adjusted equally quickly. This
feature enables the testing of components' transient response,
ensuring that they can withstand sudden environmental changes
without compromising their performance.
A sophisticated monitoring and data logging system is integrated
into the test chamber. Multiple sensors are strategically placed
throughout the chamber to continuously monitor temperature,
humidity, pressure, and other relevant parameters. The data is
logged at high frequencies, providing a detailed and continuous
record of the component's performance during the test. This data
can be analyzed in real - time or retrieved later for in - depth
post - test analysis. The comprehensive data logging capabilities
allow for the identification of potential weaknesses in the
component's design and performance, enabling manufacturers to make
informed improvements.
Given the critical nature of aircraft and satellite components, the
test chamber is built with durability and cleanliness in mind. The
chamber's exterior is constructed from high - quality, corrosion -
resistant materials that can withstand the rigors of continuous
use. The interior is designed to be clean and free from
contaminants that could potentially affect the components being
tested. Specialized air filtration and purification systems are
installed to maintain a clean environment within the chamber,
ensuring that the test results are not influenced by external
pollutants.
Safety is of utmost importance in the testing of aircraft and
satellite components. The test chamber is equipped with a
comprehensive set of safety features, including over - temperature
and over - humidity protection, fire suppression systems, and
emergency stop buttons. In case of any abnormal conditions, such as
a sudden increase in temperature or pressure, the safety systems
will automatically activate to protect the components, the testing
equipment, and the personnel. These safety features ensure a secure
testing environment for all involved.
| Model | THC-225 | THC-408 | THC-800 | THC-1000 |
| Inside dimension(W x D x H) mm | 50 x 75 x 60 | 60 x 85 x 80 | 100 x 100 x 80 | 100 x 100 x 100 |
| Outside dimension(W x D x H) mm | 75 x 165 x 170 | 85 x 175 x 190 | 125 x 190 x 190 | 125 x 190 x 210 |
| Internal material | #304 Stainless Steel |
| External material | Powder coated #304 Stainless Steel |
| Temperature range | + 150℃~ - 70 ℃ |
| Humidity range | 5% ~ 98% R. H |
| Temperature resolution ℃ | 0.01 |
| Humidity resolution % R. H. | 0.1 |
| Temperature stability ℃ | ±0.3 |
| Humidity stability % R. H. | ±2 |
| High temperature ℃ | 100 | 100 | 100 | 100 |
| Heating time (min) | 20 | 30 | 30 | 30 |
| Low temperature | 0, -40, -70 | 0, -40, -70 | 0, -40, -70 | 0, -40, -70 |
| Cooling time (min) | 20, 50, 70 | 20, 50, 70 | 20, 50, 70 | 20, 50, 70 |
| Air circulation system | Mechanical convection system |
| Cooling system | Imported compressor, fin evaporator, gas condenser |
| Heating system | Sus304 Stainless steel High-speed heater |
| Humidification system | Steam Generator |
| Humidification water supply | Reservoir, Sensor-controller solenoid valve, recovery-recycle
system |
| Controller | Touch panel |
| Electrical power requirements | Please contact us for requirements of specific models |
| Safety device | Circuit system load protection, compressor load protection, control
system load protection, humidifier load protection, overtemperature
load protection, fault warning light |
