Custom&Other Test Chambers

Combined Temperature High Altitude Low Pressure Simulation Environmental Climatic Test Chamber


Application:

Our Lab Equipment Combined Temperature High Altitude Low Pressure Simulation Environmental Climatic Test Chamber  combine Altitude and temperature to test various components and products, especially the aircraft avionics. Automatic controlled vacuum system provide a precise altitude simulated condition up to 30000 meters. Available to connect cable for the electronic performance test.

Feature:

1. Formed sheet steel exterior structure.

2. SUS#304 Stainless steel continuously seal welding, interior cabinet cover with vapor-tight liner, excellent vacuum performance.

3. High capacity vacuum pump

4. High efficient refrigeration system

5. Programmable

Standard Compliance:

GB/T2423.1-2001 , GB/T2423.2-2001 , GB10590-89 ,GB15091-89 , GB/11159-89

GB/T2423.25-1992 , GB/T2423.26-1992 , GJB150.2-86 , GJB150.3-1986, GJB360A

Product specification:

Model

6114-100

6114-225

6114-500

6114-800

6114-1000

Test Space

W x H x D(mm)

450x500x450

600x750x500

800x900x700

1000x1000x800

1000x1000x1000

External Dimension

W x H x D(mm)

1150x1750x1050

1100x1900x1200

1450x2100x1450

1550x2200x1500

1520x2280x1720

Performance parameters:

Temp. Range

 B:-20~150     C:-40~150     D:-70~150

Temp. Fluctuation

 ±0.5(atmospheric ,no load )

Temp. Deviation

 ≤±2(atmospheric ,no load )

Temp. Uniformity

 ≤±2(atmospheric ,no load )

Cooling Rate

0.8-1.2/min

Pressure Level

101kPa-0.5kPa

Pressure Reducing Time

101kPa→1.0kPa≤30min(dry )

Pressure Deviation

atmospheric -40kp;±1.8kpa;40kp-4kpa;±4.5%kpa;4kp-0.5kpa;±0.1kpa

Pressure Recovery Time

≤10KPa/min

Weight

1500kg

Pressure Altitude Reference Table:

Setting Pressure

Altitude

1.09KPa

30500m

2.75KPa

24400m

4.43KPa

21350m

11.68KPa

15250m

19.16KPa

12200m

30.06KPa

9150m

46.54KPa

6100m

57.3 KPa

4550m

69.66KPa

3050m

 


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