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Application of Fiber Grating Sensor Systems<br />

Spacecrafts<br />

Strain & temperature sensor network: 4 arrays (sensor pads) with 12 sensors<br />

• Health monitoring NASA X-38 CRV prototype for ISS<br />

Partners: IPHT & Kayser-Threde, NASA<br />

Wavelength [nm]<br />

849<br />

848<br />

847<br />

846<br />

845<br />

844<br />

SPU box<br />

(NASA<br />

standard)<br />

-0.36nm=-560µε<br />

elongated sensor<br />

compressed sensor<br />

temperature sensor<br />

1.27nm =2000µε<br />

838<br />

0 5 10 15 20 25<br />

Time [min]<br />

FBG sensor pad<br />

(2 orthogonal strain<br />

& 1 temp. sensor)<br />

test measurement<br />

FOS - 70

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