Thermal Shock Chamber

It is employed for Thermal shock test.

Hot / Temperature Range:[+65°, +220°C]

Warm/ Temperature Range:[-80°; +60°C]

Temperature accuracy: +/- 1°C

Data acquisition:

• IMC CRONOS PL8 (60 chs)

Accredited test methods:

• ESA ECSS-E-10-03A

• MIL-STD-810-C / F / G

• RTCA DO -160D

The Thermal Shock Chamber is part of the Space Qualification Laboratory (SQL).

The SQL is an ensamble of facilites aimed at supporting aerospace companies in the design, manufacturing and testing of nano and micro satellites (up to 70 Kg) and electronic and mechanical components of space, avionic and military systems, providing service activities for the qualification and acceptance to mechanical and operational environmental loads.

Test facilities and test procedures fully meet the most rigorous standard established by the European space Agency and military requirements

Specimen length [mm]: 700.0
Specimen width/dia [mm]: 1000.0
Specimen height/thk [mm]: 1400.0
Mass max. [kg]: 100.0
Higher temperature [K]: 493.15
Lower temperature [K]: 193.15
Data acquisition: IMC CRONOS PL8 60 with n. 60 PT100 channels
Cleanroom classes (ISO 14644-1):
ISO Class ≤5
ISO Class 6
ISO Class 7
ISO Class 8
ISO Class 9
Certification:
ISO/IEC 17025
ISO 9001
AS/EN/JISQ 9100
Keywords: CIRA, temperature shock testing, thermal cycling, chamber, temperature, shock, test