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Pinhole Effects on Venus Superpressure Balloon Lifetime

机译:金星超压气球寿命的针孔效应

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Experimental results are presented for a series of experiments that addressed the effect of small pinhole defects on the potential lifetime of a Venus superpressure balloon. The experiments were performed on samples of a candidate balloon envelope material through which a single small hole of 80 to 300 microns in diameter was deliberately made in each one by puncturing with a metal pin. The material was mounted horizontally in a test apparatus and then a 2-3 mm thick layer of sulfuric acid was placed on top to mimic balloon wetting at Venus. Acid penetration and damage manifested itself as a darkening of the aluminum metal and adhesive layers around the hole in the balloon material. There were no test conditions under which the acid simply fell through the pinhole due to gravity because the surface tension forces always compensated at this size. Very little acid-damaged material was observed for the smallest 80 micron pinholes while gas flowed through the hole due to balloon-like pressurization: the black spot size was approximately 0.2 mm in diameter after 6 days with 86% sulfuric acid. The damage area grew more quickly in the absence of gas flowing out of an 80 micron hole, namely at a rate of 2 mm/day. It was concluded that the flow of escaping gas out of the hole provides a substantial reduction of the rate of acid penetration and damage. Larger diameter pinholes of approximately 300 micron diameter showed larger growth rates of 0.7 mm/day with gas flow and 1.7 mm/day without. The pinhole size did not change over the duration of these experiments because the material has an outer layer of fluoropolymer film that remained intact during the process and thereby held the hole size constant. None of the damage rates measured in these experiments pose a threat to the lifetime of the balloon over the projected course of a 30 day mission because the affected area is too small to cause a structural failure either through direct damage or increased solar heating and attendant balloon pressurization leading to burst.
机译:提出了一系列实验的实验结果,该实验解决了小针孔缺损对金星超压球囊的潜在寿命的影响。在候选球囊包络材料的样品上进行实验,通过该候选球囊包络材料的样品通过其通过用金属销刺穿,在每个小孔中刻意地刻意地进行。将材料水平安装在试验装置中,然后将2-3mm厚的硫酸层置于顶部以模仿金星的润湿。酸渗透和损坏表现为铝金属和粘合剂层围绕球囊材料的孔的变暗。没有测试条件,因为由于重力,酸只落下了针孔,因为表面张力始终以这种尺寸得到补偿。对于最小的80微米针孔观察到非常少的酸损坏材料,同时由于气球的加压而流过孔的气体:用86%硫酸6天后,黑点尺寸的直径约为0.2mm。在没有气体流出80微米孔的情况下,损伤区域越来越快地增长,即以2mm /天的速度流出。得出结论是,逃逸气体流出孔的流动可大幅减少酸渗透率和损伤。大约300微米直径的较大直径针孔显示出较大的生长速率为0.7毫米/天,气流和1.7毫米/天没有。针孔大小在这些实验的持续时间内没有改变,因为该材料具有在该过程中保持完整的外层的含氟聚合物膜,从而保持孔尺寸恒定。在这些实验中测量的损伤率没有造成威胁到30天的任务的预计过程中的气球的寿命,因为受影响的区域太小而无法通过直接损坏或增加太阳能加热和伴随气球来引起结构性失败加压导致爆裂。

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