TY - JOUR
T1 - Real-time atomic oxygen detection using transition metal oxide coated hydrogen-terminated diamond surface
AU - Bolker, Asaf
AU - Gouzman, Irina
AU - Tordjman, Moshe
AU - Atar, Nurit
AU - Riggs, Brian E.
AU - Carmiel, Yacov
AU - Verker, Ronen
AU - Grossman, Eitan
AU - Kalish, Rafi
AU - Minton, Timothy K.
N1 - Publisher Copyright:
© 2026 Elsevier Masson SAS.
PY - 2026/5
Y1 - 2026/5
N2 - Atomic oxygen (AO) is a major cause for the deterioration of spacecraft materials, such as polymers, composites and optical coatings, in low Earth orbit (LEO). AO exposure can degrade thermal, mechanical, or optical system performance, potentially leading to premature mission failure. Future missions, especially for remote sensing, are designed for very low Earth orbit (VLEO) where the variations of thermospheric density and AO flux are more significant than in higher orbits. Therefore, accurate real-time assessment of the AO fluence impinging upon spacecraft surfaces becomes a crucial issue for mission success, as well as for improving current thermospheric density models. We present a compact, solid-state sensor with high sensitivity and fast response to AO. The sensor is based on two semiconductor components that exhibit unique electrical properties when assembled together: hydrogenated diamond substrate and transition-metal oxide (TMO) coating. The Diamond:H-Transitional Metal Oxide AO sensor (DiMO) was characterized using RF plasma-based and laser detonation AO facilities. Tungsten oxide, WO3, with thickness ranging from 6 nm to 30 nm was used as TMO coating of choice. The results showed a linear increase in electrical resistance as a function of AO fluence of up to 2 × 1020 O-atoms∙cm-2, as tested in a laser detonation AO beam facility. The sensitivity of the sensor was found to be tunable, ranging from 10–14 to 10–15 Ω∙O-atoms-1∙cm2, and inversely dependent on the coating thickness. This work demonstrates the potential usage of diamond-based devices for real-time AO flux monitoring. Furthermore, compact dimensions and minimal power consumption of the DiMO sensor make it an ideal low-cost solution for the emerging "new-space" era, including nanosatellites applications.
AB - Atomic oxygen (AO) is a major cause for the deterioration of spacecraft materials, such as polymers, composites and optical coatings, in low Earth orbit (LEO). AO exposure can degrade thermal, mechanical, or optical system performance, potentially leading to premature mission failure. Future missions, especially for remote sensing, are designed for very low Earth orbit (VLEO) where the variations of thermospheric density and AO flux are more significant than in higher orbits. Therefore, accurate real-time assessment of the AO fluence impinging upon spacecraft surfaces becomes a crucial issue for mission success, as well as for improving current thermospheric density models. We present a compact, solid-state sensor with high sensitivity and fast response to AO. The sensor is based on two semiconductor components that exhibit unique electrical properties when assembled together: hydrogenated diamond substrate and transition-metal oxide (TMO) coating. The Diamond:H-Transitional Metal Oxide AO sensor (DiMO) was characterized using RF plasma-based and laser detonation AO facilities. Tungsten oxide, WO3, with thickness ranging from 6 nm to 30 nm was used as TMO coating of choice. The results showed a linear increase in electrical resistance as a function of AO fluence of up to 2 × 1020 O-atoms∙cm-2, as tested in a laser detonation AO beam facility. The sensitivity of the sensor was found to be tunable, ranging from 10–14 to 10–15 Ω∙O-atoms-1∙cm2, and inversely dependent on the coating thickness. This work demonstrates the potential usage of diamond-based devices for real-time AO flux monitoring. Furthermore, compact dimensions and minimal power consumption of the DiMO sensor make it an ideal low-cost solution for the emerging "new-space" era, including nanosatellites applications.
KW - Atomic oxygen
KW - Diamond
KW - Low Earth Orbit
KW - Metal oxide coating
KW - Real-time sensing
UR - https://www.scopus.com/pages/publications/105028066688
U2 - 10.1016/j.ast.2026.111687
DO - 10.1016/j.ast.2026.111687
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AN - SCOPUS:105028066688
SN - 1270-9638
VL - 172
JO - Aerospace Science and Technology
JF - Aerospace Science and Technology
M1 - 111687
ER -