We report on the capacitively coupled O2 plasma etching of PMMA and polycarbonate (PC) with a diffusion pump. Plasma process variables were process pressure and CCP power at 5 sccm O2 gas flow rate. Characterization was done in order to analyze etch rate, etch selectivity, surface roughness, and morphology using stylus surface profilometry and scanning electron microscopy. Self bias decreased with increase of process pressure in the range of 25~180 mTorr. We found an important result for optimum pressure for the highest etch rate of PMMA and PC, which was 60 mTorr. PMMA and PC had etch rates of 0.46 and 0.28 μm/min under pressure conditions, respectively. More specifically, etch rates of the materials increased when the pressure changed from 25 mTorr to 60 mTorr. However, they reduced when the pressure increased further after 60 mTorr. RMS roughnesses of the etched surfaces were in the range of 2.2~2.9 nm. Etch selectivity of PMMA to a photoresist was ~1.5:1 and that of PC was ~0.9:1. Etch rate constant was about 0.04 μm/minW and 0.02 μm/minW for PMMA and PC, respectively, with the CCP power change at 5 sccm O2 and 40 mTorr process pressure. PC had more erosion on the etched sidewall than PMMA did. The OES data showed that the intensity of the oxygen atomic peak (777.196 nm) proportionally increased with the CCP power.

This study investigates GaAs dry etching in capacitively coupled BCl3/N2 plasma at a low vacuum pressure (>100 mTorr). The applied etch process parameters were a RIE chuck power ranging from 100~200W on the electrodes and a N2 composition ranging from 0~100% in BCl3/N2 plasma mixtures. After the etch process, the etch rates, RMS roughness and etch selectivity of the GaAs over a photoresist was investigated. Surface profilometry and field emission-scanning electron microscopy were used to analyze the etch characteristics of the GaAs substrate. It was found that the highest etch rate of GaAs was 0.4μm/min at a 20 % N2 composition in BCl3/N2 (i.e., 16 sccm BCl3/4 sccm N2). It was also noted that the etch rate of GaAs was 0.22μm/min at 20 sccm BCl3 (100 % BCl3). Therefore, there was a clear catalytic effect of N2 during the BCl3/N2 plasma etching process. The RMS roughness of GaAs after etching was very low (~3nm) when the percentage of N2 was 20 %. However, the surface roughness became rougher with higher percentages of N2.

This study investigated dry etching of acrylic in capacitively coupled SF6, SF6/O2 and SF6/CH4 plasma under a low vacuum pressure. The process pressure was 100 mTorr and the total gas flow rate was fixed at 10 sccm. The process variables were the RIE chuck power and the plasma gas composition. The RIE chuck power varied in the range of 25~150 W. SF6/O2 plasma produced higher etch rates of acrylic than pure SF6 and O2 at a fixed total flow rate. 5 sccm SF6/5 sccm O2 provided 0.11μm/min and 1.16μm/min at 25W and 150W RIE of chuck power, respectively. The results were nearly 2.9 times higher compared to those at pure SF6 plasma etching. Additionally, mixed plasma of SF6/CH4 reduced the etch rate of acrylic. 5 sccm SF6/5 sccm CH4 plasma resulted in 0.02μm/min and 0.07μm/min at 25W and 150W RIE of chuck power. The etch selectivity of acrylic to photoresist was higher in SF6/O2 plasma than in pure SF6 or SF6/CH4 plasma. The maximum RMS roughness (7.6 nm) of an etched acrylic surface was found to be 50% O2 in SF6/O2 plasma. Besides the process regime, the RMS roughness of acrylic was approximately 3~4 nm at different percentages of O2 with a chuck power of 100W RIE in SF6/O2 plasma etching.

The critical strain energy release rate and the failure mechanisms of glass-carbon epoxy resin hybrid composites are investigated in the temperature range of the ambient temperature to 80℃. The direction of laminates and the volume fraction are [(+45, -45, 0, 0) sub(2) ] sub(s), 50%, respectively. The major failure mechanisms of these composites are studied using the scanning electron microscope for the fracture surface. Results are summarized as follows: 1) The critical strain energy release rate shows a maximum at ambient temperature and it tends to decrease as temperature goes up. 2) The critical strain energy release rate increases as the content of glass increases, and especially shows dramatic increase for the high glass fiber content specimens. 3) Major failure mechanisms can be classfied such as localized shear yielding, fiber-matrix debonding, matrix micro-cracking, and fiber pull-out and/or delamination.