ESPEC
The ESPEC TSA 101 S W Thermal Shock is a thermal shock chamber. The ESPEC TSA 101 S W Thermal Shock uses AC 200V, Phase 3 power. The ESPEC TSA 101 S W Thermal Shock has a 5.5 kW refrigeration motor and a 6 kW heater.[1][2]

Thermal shock chambers generally create alternating hot and cold environments with heating and refrigeration subsystems. Thermal shock testing places a sample through repeated temperature transitions so engineers can observe cracking, delamination, seal failure, electrical drift, or other temperature driven damage mechanisms.
Thermal shock chambers are support tools rather than primary wafer processing tools. Thermal shock testing is typically used around development, qualification, reliability screening, failure analysis, and outgoing verification for components, packages, and related hardware used in semiconductor manufacturing and electronics production.
Thermal shock chambers are used to test semiconductor devices, electronic assemblies, packaged parts, sensors, connectors, and material coupons. Thermal shock testing helps reveal weaknesses associated with thermal expansion mismatch, bonding integrity, encapsulation quality, and long term reliability under abrupt temperature change.
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The ESPEC TSA 101 S W is a thermal shock chamber in the lab and support equipment category.[2][1]
The ESPEC TSA 101 S W uses AC 200V, three-phase power.[1][2]
The following facts about the TSA 101 S W Thermal Shock are absent from this record as of this revision. First-hand knowledge or a citation closes a gap; every submission is reviewed before publication.
No publicly documented production dates or lifecycle milestones (introduction, end of production, EOL) for the TSA 101 S W Thermal Shock are on record.
Answerable by: OEM historical records or a trade-press announcement
No publicly documented variants, configuration options, or revision breakpoints of the TSA 101 S W Thermal Shock are on record.
Answerable by: an OEM product catalog or an engineer who ordered or specified the tool
The control-system platform and OS era of the TSA 101 S W Thermal Shock are not on record.
Answerable by: an engineer who operated it or OEM installation records
No publicly documented failure modes or field errata for the TSA 101 S W Thermal Shock are on record.
Answerable by: a field service engineer, process engineer, or maintenance technician
The process node or technology generation of the TSA 101 S W Thermal Shock is not on record.
Answerable by: an OEM datasheet or a fab qualification report
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Last updated Oct 15, 2026.
The Applied Materials 0010-13627 is a high efficiency RF match designed for semiconductor equipment.
General referenceThe Applied Materials 0015 20064 Part is an identified component within the lab and support equipment category, used in a supporting role around semiconductor manufacturing and processing tools.
Applied Materials 0020 19652 is a retainer bracket, top match part described as for 200mm Ultim.