Test EQ

All categories
PRODUCTS
Temperature Altitude Chamber for Combined Environmental Testing

Key Advantages:

Combined temperature + altitude (low pressure) simulation

Wide temperature range: -70°C to +150°C

Pressure control from 101 kPa to ≤0.5 kPa

Stable and uniform environmental control

Programmable multi-step test profiles

Designed for continuous reliability testing

Compliant with MIL-STD-810, IEC 60068, IEC 60749

Key Specifications of Temperature Altitude Chamber:

Typical engineering parameters include:

Serial
number
Capacity ( m3 )0.1250.5120.81.02.168.9
1ModelTemperature Low
Pressure Test Chamber
EWQT125-70WEWQT512-70WEWQT800-70WEWQT1000-70WEWQT2160-70WEWQT9.0-70W
2DimensionInternal Dimension
WxHxD (mm)
500x500x500800x800x8001000x1000x8001000x1000x10001800x1000x12001730x1980x2600
External Dimension
WxHxD (mm)
900x1680x17501200x1880x20501400x2080x20501400x2180x22502200x2180x25702130x2440x4673
2PressurePressure rangeNormal pressure~0.5Kpa ( 500pa)
Pressure error≦±2kpa Ordinary pressure ~ 40kpa
≦±5kPa (40kPa to 4kPa)
≦±0.1kpa (4kPa to 1kPa )
Depressurization timeFrom site level to 15250m in 10min
From site level to 22860m in 20min
From site level to 30500m in 30min
Rapid decompression time75.2kPa~18.8kPa≦15s (Optional)
Explosive decompression time75.2kPa~18.8kPa≦0.1s (Optional)
3TemperatureTemperature range-70℃to +180℃(200℃ is Optional)
Temperature fluctuation±0.5℃
Temperature uniformity≦±2.0℃(Normal pressure, no load, constant state)
4Heating rate2℃-15℃/min(optional)
5Cooling rate3℃-15℃/min(optional)
6HeatingNoise Level
Heating/Cooling
494949494949
Cooling656568686669
7HumidityHumidity range10%RH ~98% RH
Humidity uniformity±1.0% RH
Relative humidity deviation≦±2.0 to 3.0% RH (humidity >75%RH)
≦±5.0% RH (humidity≦75%RH)
8PowerAC380V 3phase 5lines 50/60Hz
9Aprroximate weight(kg)85015001900200035009520
10Marked1、The external dimensions and noise level do not include the vacuum pump unit (operating temperature range: -40°C to +85°C).
2、Optional low-pressure and low-temperature humidity control equipment is available (Our company possesses the technical capability to simultaneously meet temperature and humidity control requirements under low-pressure conditions).
3、Other dimensions accept customize, details parameter need contact with Sales team
11We possess the technical expertise toaddress altitude test chamber control challenges.Contact our sales team for scenario-specific solutions.

Actual performance depends on chamber size, test load, heat dissipation, pressure level and environmental profile.

For procurement, TestEQ recommends specifying the required absolute pressure, temperature range, chamber volume and test profile rather than relying only on a generic altitude value.

Temperature Altitude Chamber for Combined Temperature and Altitude Testing:

A temperature altitude chamber combines controlled temperature with reduced atmospheric pressure to reproduce environmental conditions associated with high-altitude operation.

Unlike a pressure-only altitude test chamber, a temperature altitude chamber allows engineers to evaluate products under simultaneous thermal and low-pressure stress.

TestEQ temperature altitude chambers are designed for aerospace, avionics, automotive electronics, batteries, communication equipment, electronic components and other products requiring combined temperature-altitude qualification.

Programmable temperature and pressure profiles allow engineers to reproduce controlled environmental sequences such as temperature exposure, altitude operation, pressure transitions and return to normal atmospheric conditions.


What Is a Temperature Altitude Chamber?

A temperature altitude chamber is an environmental test chamber that combines temperature control with simulated high-altitude atmospheric pressure.

The chamber uses a thermal control system to regulate temperature and a pressure-control or vacuum system to regulate absolute pressure.

This combination is useful when a product may experience both thermal stress and reduced atmospheric pressure during operation, transportation or flight.

Typical controlled parameters include:

• Temperature

• Absolute pressure

• Equivalent altitude

• Temperature ramp rate

• Pressure transition rate

• Exposure duration

• Temperature-pressure sequence

• Product operating condition

• Test data

The required conditions should be determined from the applicable product specification or test standard.


Why Combine Temperature and Altitude Testing?

Testing temperature and altitude independently does not always reproduce the combined environmental stress experienced during actual operation.

At high altitude, atmospheric pressure and air density decrease. This can influence heat transfer, cooling performance, electrical behavior and mechanical pressure differences.

When temperature changes occur at the same time, the product may experience additional thermal and environmental stress.

Combined temperature-altitude testing can therefore help engineers evaluate:

• Reduced cooling performance under low pressure

• Seal and enclosure integrity

• Temperature-dependent electrical performance

• Battery thermal behavior

• Sensor stability

• Electronic component operation

• Power electronics performance

• Material and structural response

• Product operation during altitude transitions

For aerospace equipment, RTCA DO-160 Section 4 specifically addresses temperature and altitude environmental testing. The applicable category depends on the aircraft installation environment and qualification requirements.


Temperature Altitude Chamber Working Principle

A temperature altitude chamber controls two primary environmental variables.

Temperature Control

The refrigeration and heating system establishes the required thermal condition around the test article.

Pressure Control

A vacuum or pressure-control system changes the absolute pressure inside the sealed chamber.

Coordinated Control

The control system coordinates temperature and pressure according to a programmed test profile.

This allows engineers to reproduce sequences such as:

Normal Pressure → Temperature Change → Altitude Simulation → Temperature Exposure → Pressure Recovery

The exact sequence depends on the applicable qualification specification.


Temperature Altitude Chamber vs Altitude Test Chamber

Engineering FactorAltitude Test ChamberTemperature Altitude Chamber
Primary StressReduced pressureTemperature + reduced pressure
Pressure ControlYesYes
Temperature ControlOptional / configuration-dependentCore function
Primary PurposeHigh-altitude and low-pressure testingCombined temperature and altitude qualification
Main ApplicationHigh-altitude / low-pressure testingCombined environmental qualification
Typical UsersEnvironmental test labsAerospace, electronics, battery and R&D labs
Key Selection FactorRequired pressure or simulated altitudeRequired temperature range + pressure conditions

Engineering Note: The correct configuration depends on the test article, test method, temperature range, pressure requirement and qualification standard.


Why Temperature Altitude Testing Matters

At high altitudes:

  • Air density decreases → reduced cooling efficiency

  • Pressure drops → affects sealing and structure

  • Temperature varies drastically → causes material stress

These factors can lead to:

  • Electronic malfunction

  • Material deformation

  • Seal leakage

  • Battery performance degradation

Therefore, it is necessary to identify problems in advance through environmental simulation.


Temperature Altitude Testing Standards

Common standards and specifications may include:

• RTCA DO-160 Section 4 — Temperature and Altitude

• MIL-STD-810 Method 500 — Low Pressure

• IEC 60068-2-13 — Low Air Pressure

• Customer-specific aerospace or environmental qualification specifications

IEC 60068-2-13:2021 specifies low-air-pressure testing for specimens exposed to low pressure during transportation, storage or service.

RTCA states that DO-160 provides environmental test procedures for airborne equipment, and its current published material identifies DO-160G as the current listed version while noting work toward a DO-160H revision.


How to Choose a Temperature Altitude Chamber

1. Define Temperature Requirements

Identify the minimum and maximum operating or survival temperature required by the test program.

2. Define Pressure Requirements

Specify the required absolute pressure and corresponding altitude condition.

3. Define Combined Test Sequence

Determine whether temperature and pressure change simultaneously, sequentially or according to a defined aircraft or product profile.

4. Calculate Test Load

The size, mass and heat generation of the test article can affect thermal performance and recovery time.

5. Confirm Chamber Volume

Allow sufficient space for fixtures, airflow and instrumentation without selecting a chamber based only on external product dimensions.

6. Confirm the Applicable Standard

The test category and conditions should be established before the equipment is specified.

7. Plan Data Acquisition

Pressure and temperature should be monitored together so that the final test record can demonstrate the actual environmental condition.


Why TestEQ Temperature Altitude Chambers?

TestEQ develops environmental test systems around the actual engineering requirement rather than a single standard chamber size.

Configuration options can be developed around:

• Temperature range

• Pressure range

• Equivalent altitude

• Chamber volume

• Temperature ramp

• Pressure transition

• Test article

• Test standard

• Data acquisition

• Laboratory installation

For applications requiring more complex environmental profiles, TestEQ can integrate temperature and pressure control into a programmable testing system.


FAQ:

1.What is a temperature altitude chamber?

A temperature altitude chamber is an environmental test chamber that combines controlled temperature with reduced atmospheric pressure to reproduce high-altitude environmental conditions.


2.Why combine temperature and altitude testing?

Combined testing can reproduce environmental conditions that cannot be fully represented by temperature-only or pressure-only testing.


3.Can temperature and pressure be controlled simultaneously?

Yes. A properly configured system can coordinate thermal control and pressure control according to a programmed test profile.


4.What products require temperature-altitude testing?

Typical applications include aerospace equipment, avionics, electronic components, automotive electronics, batteries, sensors and communication equipment.


5.What is the difference between a temperature altitude chamber and a low-pressure chamber?

A low-pressure chamber primarily focuses on reduced atmospheric pressure. A temperature altitude chamber adds controlled temperature as a core test parameter.


6.What should I provide when requesting a quotation?

Provide the required temperature range, pressure or altitude range, chamber volume, test article, test sequence, applicable standard and any required pressure-transition or temperature-ramp conditions.


7.What products require temperature altitude chamber testing?

Temperature altitude chamber testing is commonly used for aerospace components, aircraft electronics, EV batteries, automotive electronic systems, communication devices, sensors and semiconductor components that may experience high-altitude temperature and pressure variations during operation or transportation.


8.How do I choose the right temperature altitude chamber?

Selecting a temperature altitude chamber depends on required altitude range, pressure level, temperature range, chamber volume, test standards and application requirements. Engineers should consider test specimens, cycling profiles, control accuracy and future testing needs when selecting a system.


Internal Linking Module

Recommended Equipment

Used for standalone low-pressure/high-altitude environment simulation testing, suitable for aerospace and electronic reliability verification, and supports MIL-STD and IEC 60068 standard testing.

For customized and large-volume high-altitude environmental simulation.

Used for temperature and humidity cycling and stability testing, it is a basic environmental reliability verification device and is widely used in electronics, automotive and materials testing laboratories.


Related Standards (Testing Standards)

Temperature and altitude testing for airborne equipment.

Internationally recognized environmental testing standards cover testing methods for temperature, humidity, low pressure, and comprehensive environmental stress.

The U.S. military environmental reliability testing standard is applicable to the verification of aerospace, military, and high-reliability products.


Technical Resources

This book provides an in-depth analysis of the principles, application scenarios, and failure mechanisms of high-altitude, low-pressure testing, helping engineers understand the purpose and methods of testing.

This article provides a detailed introduction to application cases and test solution designs for temperature and low-pressure combined environmental testing in the aerospace, automotive, and electronics industries.

Temperature Altitude Testing Applications

Aerospace and Avionics

Temperature-altitude testing is widely relevant to airborne equipment where temperature and pressure conditions change with aircraft altitude.

Typical test articles include:

• Avionics

• Flight-control electronics

• Navigation equipment

• Communication systems

• Sensors

• Displays

• Electronic control units

• Aerospace connectors


Automotive Electronics

Automotive electronic components may require combined environmental testing when products are expected to operate across wide temperature and elevation ranges.

Typical test articles include ECUs, sensors, power electronics and communication modules.


EV Batteries and Power Electronics

Temperature and pressure can influence battery and power-electronic thermal behavior. A combined chamber can reproduce controlled environmental conditions for engineering evaluation where altitude is part of the use case.


Electronics and Components

PCBs, connectors, sensors and electronic assemblies can be evaluated under controlled temperature and reduced pressure to identify pressure-dependent or temperature-dependent failure mechanisms.


Research and Development

Combined temperature-altitude systems are useful for R&D programs where engineers need to reproduce multiple environmental variables in a controlled laboratory environment.


Call To Action:

Request a Temperature Altitude Chamber Solution

Need to test your product under combined temperature and reduced-pressure conditions?

TestEQ provides temperature altitude chambers engineered for aerospace, avionics, automotive electronics, batteries, semiconductors and reliability testing.


Send us your test requirements, including:

• Temperature range

• Required absolute pressure or simulated altitude

• Chamber working volume

• Test specimen and heat load

• Applicable testing standard

• Required temperature and pressure profiles

Our engineering team can recommend a suitable temperature altitude chamber configuration based on your actual test conditions.


"Request a customized temperature altitude testing solution today.

Our engineering team will help you design the optimal chamber based on your application and standards.



Related Products

Ask For A Quick Quote

We will contact you within 1 working day, please pay attention to the email with
the suffix "@test-eq.com".

We will contact you within 1 working day, please pay attention to the email with the suffix "@test-eq.com".

Company
Name*
Phone
E-Mail*
Nation
Message
By selecting the ‘I agree’ button, you consent to the processing of your personal data for marketing purposes and for the sending of commercial information by TESTEQ Company through telephone, e-mail, newsletters, text messages such as sms, chat and social networks.
I AGREE
By submitting your personal data, you declare that you have read the Privacy Policy of the website.

P.IVA: 91441900MAECQJHY37 Guangdong Test EQ Equipment Co., Ltd. | All Rights Reserved