首页> 外文会议>Advances in Resist Technology and Processing XIX >Defect Density Control on 'Satellite Spots' or Chemical Stains for Deep-UV Resist Process
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Defect Density Control on 'Satellite Spots' or Chemical Stains for Deep-UV Resist Process

机译:控制“卫星斑点”或化学污渍以进行深紫外线抵抗工艺的缺陷密度控制

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Satellite spots defects of size less than lum are being experienced with deep-UV photo resists at Chartered and it is believed to be formed as a result of the insoluble resist residue remaining on the BARC after the developing process. Though these defects reported are by far "cosmetic" defects that are not transferred after etch, the overwhelming number of "satellite spots" can be a nuisance to any Yield engineer from the Defect Density group as they often 'mask' away the genuine "killer" defects. Nonetheless, we expect the results presented here to be significant and recommendations made applicable to smaller geometries and to 12-inch wafer fabs. Figure 1 shows a typical "satellite spots" defect found in the open area where there are no resist patterns after the developing process. The effect of the developer/surfactant concentration is believed to have caused the polymer to form micelles during development termed affectionately as "satellite spots" defect by the Yield Engineers. In a small geometry on a patterned wafer under microgravity environment, the thin resist-developer dissolution during the developing cycle, causes the micro "dry" spots in the dissolution under the spreading developer probably due to Marangoni effect, The high surface tension of the deep-UV resists is believed to make it more difficult to remove after the hard bake process. The probabilistic model for the mechanism of resist-developer dissolution provides a theoretical understanding and leads to the resolution of "satellite spots" defect. It adequately accounts for the dissolution behaviour of the HS/TBA copolymers (ESCAP-type) resist. Different developing recipes ranging from DI-water pre-wet, developer pre-wet, to high spin speed during DIW rinse were being investigated to find out the effectiveness in removing satellite spots. The combination of extended DIW rinse time, without resorting to high spin speed or high acceleration, and "double developer puddling" programs produce the lowest counts with the TMAH developer. Considerable defect density improvement after modifying the developing program can be realized using the above control methodology.
机译:特许半导体公司的深紫外光致抗蚀剂正在经历尺寸小于lum的卫星斑点缺陷,据信这是由于显影过程后残留在BARC上的不溶性抗蚀剂残留物而形成的。尽管到目前为止报告的这些缺陷是“美容”缺陷,它们在蚀刻后不会转移,但是“缺陷点”数量巨大,对于缺陷密度小组的任何良率工程师来说都是一个麻烦,因为它们经常“掩盖”真正的“杀手er” ”缺陷。尽管如此,我们希望这里提出的结果将是有意义的,并提出适用于较小几何尺寸和12英寸晶圆厂的建议。图1示出了在显影过程之后在没有抗蚀剂图案的开放区域中发现的典型的“卫星斑点”缺陷。据信显影剂/表面活性剂浓度的影响已导致聚合物在显影过程中形成胶束,被亲爱的工程师称为亲爱的“卫星斑点”缺陷。在微重力环境下,在已图案化晶圆上的小几何形状中,显影周期中稀薄的抗蚀剂-显影剂溶解,可能是由于Marangoni效应而在展开的显影剂下在溶解中产生了微小的“干燥”斑点,深层的高表面张力-UV抗蚀剂被认为使得在硬烘烤过程之后更难以去除。抗蚀剂-显影剂溶解机理的概率模型提供了理论上的理解,并导致“卫星斑点”缺陷的解决。它充分说明了HS / TBA共聚物(ESCAP型)抗蚀剂的溶解行为。研究了不同的显影配方,从去离子水预湿,显影剂预湿到去离子水冲洗过程中的高速旋转,以发现去除卫星斑点的有效性。延长DIW冲洗时间(不求助于高旋转速度或高加速度)和“双重显影剂冲洗”程序的组合,使用TMAH显影剂的计数最少。使用上述控制方法可以在修改显影程序后显着提高缺陷密度。

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