Strain and temperature monitoring in composite sandwich panels in space environment

Shigenori Kabashima

doi:10.1117/12.2302191

9 November 2000 Strain and temperature monitoring in composite sandwich panels in space environment

Shigenori Kabashima

Proceedings Volume 4185, Fourteenth International Conference on Optical Fiber Sensors; 41851C (2000) https://doi.org/10.1117/12.2302191
Event: Fourteenth International Conference on Optical Fiber Sensors, 2000, Venice, Italy

Abstract

To develop a health monitoring system for satellite, FBG sensor was applied to a composite panel with heat-pipe. Temperature and strain in the panel were successfully measured during thermallvacuum test in a vacuum thermal chamber.

Citation Download Citation

Shigenori Kabashima "Strain and temperature monitoring in composite sandwich panels in space environment", Proc. SPIE 4185, Fourteenth International Conference on Optical Fiber Sensors, 41851C (9 November 2000); https://doi.org/10.1117/12.2302191

ACCESS THE FULL ARTICLE

INSTITUTIONAL
Select your institution to access the SPIE Digital Library.

SELECT YOUR INSTITUTION

PERSONAL
Sign in with your SPIE account to access your personal subscriptions or to use specific features such as save to my library, sign up for alerts, save searches, etc.

PERSONAL SIGN IN

No SPIE Account? Create one

PURCHASE THIS CONTENT

SUBSCRIBE TO DIGITAL LIBRARY

50 downloads per 1-year subscription

Members: $195

Non-members: $335 ADD TO CART

25 downloads per 1 - year subscription

Members: $145

Non-members: $250 ADD TO CART

PURCHASE SINGLE ARTICLE

Includes PDF, HTML & Video, when available