Graded-Compliance Metal-Packaged FBG Strain Sensor for Cryogenic Strain Measurement of Reusable Launch Vehicles

This study develops a graded-compliance, metal-packaged fiber Bragg grating (FBG) strain sensor for cryogenic structural health monitoring of metallic propellant tanks and pipelines on reusable launch vehicles (RLVs). The serially connected frame enables customizable sensitivity and expands the effective measurement range via strain desensitization for large-magnitude cryogenic strains. This design reduces interfacial shear stress and improves long-term stability under cyclic cryogenic loads, while glass brazing fixation avoids the failures associated with organic adhesives. The ground characterizations down to 77 K show high linearity (R2 > 0.998) over −4000 to 6000 με. The tensile sensitivity decreases by approximately 4.3% from room temperature to 77 K, with a tension–compression sensitivity discrepancy of 2.4% under cryogenic conditions. The limited sensitivity drift across 77 K–123 K and favorable batch consistency support a unified full-temperature-range sensitivity calculation method, reducing the onboard computational burden. Within the cryogenic operating range of 77 K–123 K, the maximum full-scale error is ±1.01%. Batch-produced sensors have passed environmental qualification tests, and units from different batches were deployed in three independent RLV flight campaigns in 2024, 2025, and 2026. Continuous and stable strain signals were obtained during ground propellant loading and in-flight phases under severe thermo-mechanical loads, consistent with the theoretical predictions.

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Publication Details

Journal
Aerospace
Published
2026-11-03
DOI
https://doi.org/10.3390/aerospace13111019
Primary Topic
Advanced Fiber Optic Sensors
Type
article
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article

Graded-Compliance Metal-Packaged FBG Strain Sensor for Cryogenic Strain Measurement of Reusable Launch Vehicles

Huiwen Niu, Jiachen Ning, Zhoulu Sun, Yu Yang et al.
Aerospace
Advanced Fiber Optic Sensors
article

Graded-Compliance Metal-Packaged FBG Strain Sensor for Cryogenic Strain Measurement of Reusable Launch Vehicles

Huiwen Niu, Jiachen Ning, Zhoulu Sun, Yu Yang, Yan Yang, Kaixiang Gong, Yongqing Peng, Zhaogang Wang, Tao Liu
article en

Abstract

This study develops a graded-compliance, metal-packaged fiber Bragg grating (FBG) strain sensor for cryogenic structural health monitoring of metallic propellant tanks and pipelines on reusable launch vehicles (RLVs). The serially connected frame enables customizable sensitivity and expands the effective measurement range via strain desensitization for large-magnitude cryogenic strains. This design reduces interfacial shear stress and improves long-term stability under cyclic cryogenic loads, while glass brazing fixation avoids the failures associated with organic adhesives. The ground characterizations down to 77 K show high linearity (R2 > 0.998) over −4000 to 6000 με. The tensile sensitivity decreases by approximately 4.3% from room temperature to 77 K, with a tension–compression sensitivity discrepancy of 2.4% under cryogenic conditions. The limited sensitivity drift across 77 K–123 K and favorable batch consistency support a unified full-temperature-range sensitivity calculation method, reducing the onboard computational burden. Within the cryogenic operating range of 77 K–123 K, the maximum full-scale error is ±1.01%. Batch-produced sensors have passed environmental qualification tests, and units from different batches were deployed in three independent RLV flight campaigns in 2024, 2025, and 2026. Continuous and stable strain signals were obtained during ground propellant loading and in-flight phases under severe thermo-mechanical loads, consistent with the theoretical predictions.

AerospaceVol. 13(11)
China Academy of Launch Vehicle Technology (CN)
Openalex Percentile: Top 26%
Advanced Fiber Optic Sensors
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Graded-Compliance Metal-Packaged FBG Strain Sensor for Cryogenic Strain Measurement of Reusable Launch Vehicles — Huiwen Niu, Jiachen Ning, et al. · Aerospace (2026) | TGRS Research Map | TGRS