Abstract

SiC wafers were etched using a filament plasma of He:NF3:O2 (helium:nitrogen trifluoride:oxygen) mixed gas at atmospheric pressure. When 0.5–2 sccm of NF3 was mixed to 2 slm of He filament plasma, the etch depth and etch rate increased, but there was little change in the etch width as the NF3 mixing amount increased. The increment of the NF3 mixing also suppressed the surface roughening of plasma etching. The addition of O2 to the He-NF3 filament plasma slightly increased the SiC wafer etch rate. When the NF3 mixing amount was 2 sccm, the roughness of the etched surface increased sharply by O2 addition. On the contrary, the NF3 mixing amount was 1 sccm; the addition of O2 reduced the roughness more than that of the pristine. The roughness of the pristine SiC wafer specimens is in the range of Ra 0.7–0.8 nm. After 30 min of etching on a 6 mm by 6 mm square area, the roughness of the etched surface reduced to Ra 0.587 nm, while the etch rate was 2.74 μm/h with a He:NF3:O2 of 2:1:3 (slm:sccm:sccm) filament plasma and 3 mm/s speed of raster scan etch of the optimized roughening suppression etching recipe.

Highlights

  • The silicon carbide (SiC) material is used for the mirrors of space telescopes and molds for glass optics manufacturing, due to the superb characteristics of high hardness, chemical inertness, and its low specific gravity [1,2,3]

  • The characteristics of the filament plasma generated between the plasma module and SiC wafer using He-NF3 mixed gas were examined

  • The filament plasma in normal filament (NF) mode is developed normally on the surface of the SiC wafer, which is suitable for the etching process

Read more

Summary

Introduction

The silicon carbide (SiC) material is used for the mirrors of space telescopes and molds for glass optics manufacturing, due to the superb characteristics of high hardness, chemical inertness, and its low specific gravity [1,2,3]. The Young’s modulus/Vickers hardness and tensile strength/shear strength ratio are about 20 and 1.5, and those are very low comparing with metals of about 250 and 10, respectively. For these reasons, it is very hard to apply the conventional metal machining method for SiC material [8]. Conventional machining methods such as grinding, lapping, and chemical mechanical polishing (CMP) are used for manufacturing the SiC mirror, but it takes enormous time and energy, leaving lots of surface damages such as scratches, subsurface damage (SSD), and micro pits by the machining tools, which has an adverse effect on the telescope performance [12,13,14,15,16,17,18]. Due to the need for the free-form machining, the existing methods require a lot of time-consuming additional correction machining

Methods
Results
Conclusion
Full Text
Published version (Free)

Talk to us

Join us for a 30 min session where you can share your feedback and ask us any queries you have

Schedule a call