Repeatability Measurements of Apparent Thermal Conductivity of Multilayer Insulation (MLI)

Cryogenic Engineering Conference 2017

材料科学;物理学

Vanderlaan, M.^1,2 ; Stubbs, D.^1,2 ; Ledeboer, K.^1,3 ; Ross, J.^1,2 ; Van Sciver, S.^1,2 ; Guo, W.^1,2

National High Magnetic Field Laboratory, Tallahassee

FL, United States^1

Mechanical Engineering Dept., FAMU-FSU College of Engineering, Tallahassee

FL, United States^2

University of Twente, Enschede, Netherlands^3

关键词: Apparent thermal conductivity;    Boundary temperature;    Concentric cylinders;    Lower temperatures;    Measurements of;    Multi-layer insulation;    Test condition;    Thermal conductivity measurements;   

Others  :  https://iopscience.iop.org/article/10.1088/1757-899X/278/1/012195/pdf
DOI  :  10.1088/1757-899X/278/1/012195

学科分类：材料科学（综合）

来源: IOP

【 摘 要 】

This report presents and discusses the results of repeatability experiments gathered from the multi-layer insulation thermal conductivity experiment (MIKE) for the measurement of the apparent thermal conductivity of multi-layer insulation (MLI) at variable boundary temperatures. Our apparatus uses a calibrated thermal link between the lower temperature shield of a concentric cylinder insulation assembly and the cold head of a cryocooler to measure the heat leak. In addition, thermocouple readings are taken in-between the MLI layers. These measurements are part of a multi-phase NASA-Yetispace-FSU collaboration to better understand the repeatability of thermal conductivity measurements of MLI. NASA provided five 25 layer coupons and requested boundary temperatures of 20 K and 300 K. Yetispace provided ten 12-layer coupons and requested boundary temperatures of 77 K and 293 K. Test conditions must be met for a duration of four hours at a steady state variance of less than 0.1 K/hr on both cylinders. Temperatures from three Cernox® temperature sensors on each of the two cylinders are averaged to determine the boundary temperatures. A high vacuum, less than 10-5torr, is maintained for the duration of testing. Layer density varied from 17.98 - 26.36 layers/cm for Yetispace coupons and 13.05 - 17.45 layers/cm for the NASA coupons. The average measured heat load for the Yetispace coupons was 2.40 W for phase-one and 2.92 W for phase-two. The average measured heat load for the NASA coupons was 1.10 W. This suggests there is still unknown variance of MLI performance. It has been concluded, variations in the insulation installation heavy effect the apparent thermal conductivity and are not solely dependent on layer density.