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NASA NTRS · 20090040060

Cryogenic Chamber for Servo-Hydraulic Materials Testing

Abstract

A compact cryogenic test chamber can be cooled to approximately 5 to 6 Kelvin for materials testing. The system includes a temperature controller and multiple sensors to measure specimen temperature at different locations. The testing chamber provides a fast and easy method to perform materials testing at lower than liquid nitrogen temperature (77 K). The purpose of the chamber is to cool a composite lap shear specimen to approximately 20 K so that tensile test force and displacement data may be acquired at this cryogenic temperature range.

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BibTeXRIS

Francis, John J., Tuttle, James. 2009-11-01. Cryogenic Chamber for Servo-Hydraulic Materials Testing. https://ntrs.nasa.gov/citations/20090040060

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