| Literature DB >> 33435433 |
Xiangyu Yang1, Wenping Geng1, Kaixi Bi1, Linyu Mei2, Yaqing Li1, Jian He1, Jiliang Mu1, Xiaojuan Hou1, Xiujian Chou1.
Abstract
In situ measurements of sensing signals in space platforms requires that the micro-electro-mechanical system (MEMS) sensors be located directly at the point to be measured and in contact with the subject to be measured. Traditional radiation-tolerant silicon-based MEMS sensors cannot acquire spatial signals directly. Compared to silicon-based structures, LiNbO3 single crystalline has wide application prospects in the aerospace field owing to its excellent corrosion resistance, low-temperature resistance and radiation resistance. In our work, 4-inch LiNbO3 and LiNbO3/Cr/Au wafers are fabricated to silicon substrate by means of a polyimide bonding method, respectively. The low-temperature bonding process (≤100 °C) is also useful for heterostructure to avoid wafer fragmentation results from a coefficient of thermal expansion (CTE) mismatch. The hydrophilic polyimide surfaces result from the increasing of -OH groups were acquired based on contact angle and X-ray photoelectron spectroscopy characterizations. A tight and defect-free bonding interface was confirmed by scanning electron microscopy. More importantly, benefiting from low-temperature tolerance and radiation-hardened properties of polyimide material, the bonding strength of the heterostructure based on oxygen plasma activation achieved 6.582 MPa and 3.339 MPa corresponding to room temperature and ultra-low temperature (≈ -263.15 °C), which meets the bonding strength requirements of aerospace applications.Entities:
Keywords: LiNbO3 single crystalline; low-temperature bonding; low-temperature tolerance; oxygen plasma activation; polyimide material; radiation-hardened properties
Year: 2021 PMID: 33435433 PMCID: PMC7826505 DOI: 10.3390/mi12010070
Source DB: PubMed Journal: Micromachines (Basel) ISSN: 2072-666X Impact factor: 2.891