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Thermal Vacuum Test Chamber for Space Simulation & Aerospace Testing

Key Advantages:

Capacity:0.5 m³ to 2.65 m³(Customizable)

High Vacuum Level (mbar):1.0×10⁻⁷

No-load Vacuum Level (mbar):5×10⁻⁷ mbar(Room temperature)

Vacuum Cube Leak Rate:1×10−9std/cc/sec

Temperature Range: -190°C(LN2 cooling) to 200°C

Temperature Uniformity:±2℃

Patent Number: CN202510795397.6

Stable pressure control across multiple vacuum ranges

Designed for space simulation and aerospace qualification

Supports thermal cycling under vacuum conditions


Key Specifications of Thermal Vacuum Test Chamber:

Serial
number
Capacity ( m3 )0.4020.7852.65
1Model EZKT 1000-5EZKT 1200-5EZKT 1700-5
2Thermal Shroud
Internal Dimensions (mm)
(straight cylindrical section)
ø 800×800 ø 1000×1000 ø 1500×1500 
3Vacuum Chamber
Internal Dimensions (mm)
(straight cylindrical section)
ø 1000×1000 ø 1200×1200 ø 1700×1700 
4Thermal Plate Dimensions (mm)600×500800×7001300×1200
5High Vacuum Level1.0×10−7 Torr(1.33×10−7 mbar)
6No-load Vacuum Level (mbar)5.0×10−7(Room temperature)
7Pressure Regulation
in Multiple Ranges (mbar/Torr)
Stable pressure operation under the following levels
1.0×10-2 , 1.0×10-3 , 1.0×10-4 , 1.0×10-5 , 1.0×10−6 (Room temperature)
8Vacuum Cube Leak Rate≤ 1×10-9 std/cc/sec
9Refrigeration ModeA:Thermal sink + Cold plate
B:Thermal sink +Heating cage
C: Liquid nitrogen thermal sink+ Heating cage
10Temperature Range

Gaseous Nitrogen Control:  -180°C to 200°C 

Mechanical Refrigeration:   -80°C to 150°C 

Flooded Liquid Nitrogen :  -190°C

11Temperature Uniformity±2℃
(Measured at any point on the heat sink
and cold plate under stable conditions
in a vacuum environment)
12Temperature Rising /
Falling Speed Rate
 -70℃  to 100℃ ≥ 3℃/min
 100℃  to -50℃ ≥ 3℃/min  (By Mechaincal cooling)
13Temperature Rising /
Falling Speed Rate  -Optional
 -150℃  to 125℃ ≥ 3℃/min
 125℃  to -150℃ ≥ 3℃/min  (By pressurized GN2 reciculation)
14Vacuum Acquisition System Mechanical Pump / Roots Pump / Molecular Pump / Cryopump
15PowerAC380V 3phase 5lines  50/60Hz
16We possess the technical expertise to address integrated temperature-humidity control challenges
in low-pressure environments. Contact our sales team for scenario-specific solutions.

 Opening:

The Thermal Vacuum Test Chamber (TVAC) is designed to simulate the extreme conditions of outer space by combining high vacuum and wide temperature ranges in a controlled environment.

By recreating vacuum conditions and thermal cycling simultaneously, it enables accurate testing of satellites, aerospace components, and high-reliability electronics before deployment. This testing is essential to ensure performance in space, where hardware must operate under high vacuum and extreme thermal fluctuations


Working Principle:

The chamber combines:

  • Vacuum pumping system (to achieve ultra-low pressure)

  • Thermal shroud or cold plate (for temperature control)

  • Heating system (for high-temperature simulation)

Under vacuum conditions, heat transfer occurs mainly through radiation instead of convection, accurately replicating space environments where air is absent.


Designed for Space Simulation Testing:

Thermal vacuum testing enables engineers to evaluate:

  • Thermal deformation of structures

  • Material outgassing behavior

  • Electronic performance under vacuum

  • Thermal balance and heat dissipation

This process is essential for pre-launch qualification of aerospace systems and ensures mission reliability.


Thermal Vacuum vs Thermal Cycling:


FeatureThermal VacuumThermal Cycling
EnvironmentVacuum + temperatureAir environment
Heat TransferRadiationConvection
ApplicationSpace & aerospaceElectronics
StandardECSS / MIL-STD-1540JESD22


Why Choose TestEQ:

  • Expertise in advanced environmental simulation systems

  • Proven solutions for aerospace & high-end laboratories

  • Stable vacuum and thermal control technology

  • Custom engineering for complex testing requirements

  • Reliable performance under extreme conditions


Optional Configurations

  • Liquid nitrogen cooling (LN₂ boost to -190°C)

  • Solar radiation simulation system

  • Multi-zone thermal control

  • Large-scale customized chambers

  • Remote monitoring & data acquisition system


FAQ:

What is a thermal vacuum test chamber?

A thermal vacuum chamber simulates space conditions by combining high vacuum and extreme temperature environments for reliability testing.


What is thermal vacuum testing used for?

It is mainly used for satellite, aerospace, and space electronics testing before launch.


What vacuum level is required for space simulation?

Typical thermal vacuum testing requires vacuum levels around 10⁻⁶ to 10⁻⁷ mbar depending on application.


What is the difference between thermal vacuum and thermal shock?

Thermal vacuum combines vacuum + temperature, while thermal shock focuses on rapid temperature change only.


How to choose a thermal vacuum chamber?

Key factors include:

Vacuum level

Temperature range

Chamber size

Test standards

Application (satellite, materials, electronics)


Standards Supported

1.Military:

MIL-STD-810H (Method 501.7, 502.6), MIL-STD-1540E (Space Vehicle Requirements).


2.European Space:

ECSS-E-ST-10-03C (Thermal Vacuum Testing), ECSS-Q-ST-70-02C (Contamination Control).


3.Commercial:

NASA-HDBK-6022 (Materials Compatibility), ISO 14644-1 (Cleanroom Class 100–100,000).


4.Industry-Specific:

GSFC-STD-7000 (Goddard Space Flight Center), JAXA-STD-003 (Japan Aerospace).


Applications:

This thermal vacuum chamber is widely used in:

  • Satellite and spacecraft testing

  • Aerospace component validation

  • Space electronics and payload testing

  • Material outgassing and vacuum compatibility testing

  • Optical systems and sensor calibration

  • Battery and thermal management system testing

 Thermal vacuum testing is critical for verifying spacecraft performance before launch and ensuring reliability in space environments


Call To Action:


"Request a customized thermal vacuum testing solution today

Our engineers will help you design a chamber tailored to your aerospace or laboratory requirements.

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