S&T

The DO 160 H / -60 G testing equipment is designed for environmental testing of aircraft and aircraft components.

This equipment is primarily used to evaluate the durability and safety of aircraft electronic equipment and systems.

DO-160 is an international standard that defines the environmental requirements for aviation electronics, and this testing equipment is designed to perform tests that meet this standard.

In particular, DO-160 H and DO-160 G are important for evaluating equipment performance in extreme environments such as temperature, humidity, and vibration. DO-160 H: A standard that verifies whether aviation electronic equipment operates properly at extreme temperatures and altitudes.

This standard includes testing for various environmental factors such as temperature, humidity, atmospheric pressure, vibration, and shock. DO-160 G: A standard that defines testing for mechanical environments such as vibration and shock.

This standard tests whether equipment can withstand various vibrations and shocks that may occur during flight.

Key Features

Precise Temperature Control The DO 160 H test covers a very wide temperature range, and various tests from high to low temperatures can evaluate whether equipment operates well in extreme environments.

Various Environmental Simulations Can simulate various environments including humidity, vibration, and atmospheric pressure, testing multiple conditions that equipment may experience in actual aircraft.

Vibration and Shock Durability Testing The DO 160 G test evaluates durability against vibration and shock, testing whether aircraft electronic equipment can withstand mechanical stress that may occur during flight.

Altitude and Power Testing Tests verify whether equipment operates normally in environments considering altitude and atmospheric pressure, and also checks performance related to power supply.

Automated Test Progression The testing equipment conducts tests according to the configured conditions through an automated control system and records and analyzes test data in real time.

Test Temperature Range	-55°C ~ +85°C (some tests support a wider range)
Humidity Test	Settable up to 95% RH (relative humidity)
Vibration Test	Vibration frequency range: 5 Hz ~ 500 Hz; adjustable frequency and intensity
Atmospheric Pressure	Altitude simulation: up to 30,000 ft (including pressure variation)
Power	DC power supply: 28 V DC (aircraft power standard)
Shock Test	Supports shock testing up to 50 g
Data Logging	Automatic data logging during testing with result analysis support
Safety Features	Overheat protection system, automatic test termination, and other integrated safety devices

Software Support Specifications

Test Automation Automation of test setup, start, termination, and control.

Remote Control Remote control and monitoring of testing equipment.

Data Collection and Analysis Test results are automatically saved in CSV, Excel, and PDF formats, with subsequent report generation.

Provides statistical analysis including average values, maximum values, and more.

Real-Time Monitoring Real-time verification of HRR, smoke density, oxygen consumption rate, and more. Real-time measurement of HRR (Heat Release Rate), smoke density, and gas concentration, displayed in graph form.

Error Detection and Warning Provides warning messages when abnormalities occur during testing.

The DO 160 H / -60 G testing equipment is designed for environmental testing of aircraft and aircraft components. This equipment is primarily used to evaluate the durability and safety of aircraft electronic equipment and systems. DO-160 is an international standard that defines the environmental requirements for aviation electronics, and this testing equipment is designed to perform tests that meet this standard. In particular, DO-160 H and DO-160 G are important for evaluating equipment performance in extreme environments such as temperature, humidity, and vibration. DO-160 H: A standard that verifies whether aviation electronic equipment operates properly at extreme temperatures and altitudes. This standard includes testing for various environmental factors such as temperature, humidity, atmospheric pressure, vibration, and shock. DO-160 G: A standard that defines testing for mechanical environments such as vibration and shock. This standard tests whether equipment can withstand various vibrations and shocks that may occur during flight.

Key Features

Precise Temperature Control The DO 160 H test covers a very wide temperature range, and various tests from high to low temperatures can evaluate whether equipment operates well in extreme environments.

Various Environmental Simulations Can simulate various environments including humidity, vibration, and atmospheric pressure, testing multiple conditions that equipment may experience in actual aircraft.

Vibration and Shock Durability Testing The DO 160 G test evaluates durability against vibration and shock, testing whether aircraft electronic equipment can withstand mechanical stress that may occur during flight.

Altitude and Power Testing Tests verify whether equipment operates normally in environments considering altitude and atmospheric pressure, and also checks performance related to power supply.

Automated Test Progression The testing equipment conducts tests according to the configured conditions through an automated control system and records and analyzes test data in real time.

Test Temperature Range	-55°C ~ +85°C (some tests support a wider range)
Humidity Test	Settable up to 95% RH (relative humidity)
Vibration Test	Vibration frequency range: 5 Hz ~ 500 Hz; adjustable frequency and intensity
Atmospheric Pressure	Altitude simulation: up to 30,000 ft (including pressure variation)
Power	DC power supply: 28 V DC (aircraft power standard)
Shock Test	Supports shock testing up to 50 g
Data Logging	Automatic data logging during testing with result analysis support
Safety Features	Overheat protection system, automatic test termination, and other integrated safety devices

Software Support Specifications

- Test Automation Automation of test setup, start, termination, and control.

- Remote Control Remote control and monitoring of testing equipment.

- Data Collection and Analysis Test results are automatically saved in CSV, Excel, and PDF formats, with subsequent report generation. Provides statistical analysis including average values, maximum values, and more.

- Real-Time Monitoring Real-time verification of HRR, smoke density, oxygen consumption rate, and more. Real-time measurement of HRR (Heat Release Rate), smoke density, and gas concentration, displayed in graph form.

- Error Detection and Warning Provides warning messages when abnormalities occur during testing.

Equipment Specifications