Measurement of Low Thermal Conductivity using New Correction Method under Vacuum

Author:

Tomioka Kota1,Ozeki Shuntaro1,Tachikawa Sumitaka2,Omura Takahiro3,Nagasaka Yuji4

Affiliation:

1. School of Integrated Design Engineering, Graduate School of Science and Technology, Keio University

2. Japan Aerospace Exploration Agency, Institute of Space and Astronautical Science

3. RD Dept. Intelligent Mechanical Engineering, National Institute of Technology, Wakayama College

4. Dept. of System Design Engineering, Fac. of Science and Technology, Keio University

Publisher

The Japan Society of Thermophysical Properties

Subject

General Medicine

Reference9 articles.

1. [1] D. G. Gilmore, “Spacecraft Thermal Control Handbook Volume I: Fundamental Technologies”, (2002) 167, The Aerospace Corporation.

2. [2] S. Tachikawa, R. Takagi, Y. Mizutani, Y. Hiasa, A. Ohnishi, “Performance Evaluation of New Thermal Insulation System with Polyimide Foams”, Proc. 41st International Conference on Environmental Systems, (2011) AIAA 2011-5257.

3. [3] K. Tomioka, S. Tachikawa, K. Kawahara, Y. Nagasaka, “Radiowave Transmissive MLI with Dielectric Multilayer Films”, Proc. 61st Space Sciences and Technology Conference, (2017) 3F16.

4. [4] K. Tomioka, S. Tachikawa, K. Kawahara, Y. Nagasaka, “Design and measurement of radiowave transmissive thermal control mirror”, J. Spacecraft and Rockets, 53-6 (2016) 1043-1050.

5. [5] T. Ohmura, “Measurement Error Reduction Method for Thermal Conductivity of Thermal Insulations Using GHP Method”, Proc. 3rd International Forum on Heat Transfer, (2012).

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