Abstract
Photonic integrated circuits (PICs) offer a pathway to miniaturized fiber Bragg grating (FBG) interrogators for structural health monitoring aboard satellites. However, the environmental resilience of PIC-based components remains insufficiently investigated compared to their discrete counterparts. This study reports the environmental testing of a silicon oxynitride arrayed waveguide grating (AWG) as a key component of an FBG interrogator, and presents an interrogator layout designed for the CubeSat form-factor. Vibration testing under Soyuz-2 launch profiles for secondary payloads confirmed the structural integrity of the AWG, with no performance degradation observed. Thermal vacuum cycling of AWG (−20°C to +80°C) revealed a linear spectral shift of (+11 ± 1) pm/°C across its channels, which is algorithmically compensable. γ-irradiation with a total ionizing dose of 2.8 krd induced a mean spectral shift of 63 pm in the AWG channels, indicating the necessity for radiation hardening measures. The presented study demonstrates the viability of AWG-based FBG interrogators for space applications.
| Original language | English |
|---|---|
| Article number | 30011 |
| Journal | Chinese Optics Letters |
| Volume | 24 |
| Issue number | 3 |
| DOIs | |
| State | Published - 10 Mar 2026 |
Keywords
- CubeSat
- arrayed waveguide grating
- fiber Bragg grating
- integrated photonics
- interrogator
- space qualification
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