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A Nichrome Burn Wire Release Mechanism for CubeSats

机译:用于立方体卫星的镍铬烧伤线释放机制

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The nichrome bum wire release mechanism uses a nichrome burn wire which when activated heats up and cuts through a Vectran tie down cable allowing the deployable on the satellite to actuate. The release mechanism was designed from scratch with the goals to make it small, inexpensive, simple, reliable and easy to use by anyone including student-run University CubeSat projects. The release mechanism, shown in Figure 1, utilizes a two saddle design with compression springs to apply a spring stroke and force to the nichrome wire to thermally cut through the Vectran cable when heated. Through a test program and using a design of experiments (DOE) approach it was determined that the applied current to the nichrome wire and the diameter of the nichrome wire were the key parameters governing successful performance. To activate the nichrome wire a constant current of 1.60 ± 0.05 amps is applied to ensure a successful and reliable cut. The tight tolerance constant current source is necessary in order to reliably: 1.) thermally cut the cable and 2.) prevent overheating failure of the nichrome wire to allow the mechanism to be reusable for many actuations without replacing the nichrome filament. The tight tolerances on the current prevent failure of the nichrome wire from overheating under too much current in a vacuum while also providing adequate thermal margin to cut through the Vectran tie down cable in air which requires more current than in vacuum. The burn wire release mechanism has been tested in air at room temperature and in vacuum at temperatures as low as -50°C and as high as 70°C on two different Vectran cable thicknesses. The release mechanism has shown to have cut times ranging from 2.4 to 7.2 seconds under these operating conditions. The burn wire release mechanism has 400 firings in component and system level testing without a single failure. The mechanism has been qualified for flight on the TEPCE (Tether Electrodynamic Propulsion CubeSat Experiment) program to release two carpenter tape deployments and a stacer and tether deployment system.
机译:镍铬烙铁丝释放机构使用镍铬合金烧伤丝,当激活时,镍铬丝烧伤并切断Vectran束缚电缆,从而使卫星上的可展开物致动。发行机制的设计是从零开始的,目标是使其小型,廉价,简单,可靠且易于使用,包括由学生管理的University CubeSat项目在内的任何人。如图1所示,释放机构采用带有压缩弹簧的两个鞍形设计,以对镍铬合金丝施加弹簧行程和力,使其在加热时通过Vectran电缆进行热切割。通过测试程序并使用实验设计(DOE)方法,可以确定施加到镍铬合金丝的电流和镍铬合金丝的直径是控制成功性能的关键参数。为了激活镍铬合金丝,需要施加1.60±0.05安培的恒定电流,以确保切割成功且可靠。为了可靠地使用,必须具有严格的公差恒定电流源:1.)热切割电缆,并且2.)防止镍铬合金线过热故障,以使该机构可重复使用多次,而无需更换镍铬合金灯丝。电流的严格公差可防止镍铬合金丝在真空中有太多电流时因过热而失效,同时还提供了足够的热裕度以切断空气中比真空中需要更多电流的Vectran束缚电缆。在两种不同的Vectran电缆厚度下,在室温,低至-50°C和高至70°C的温度下,在空气中,室温下和真空中,测试了灼热丝释放机构。在这些操作条件下,释放机构的切断时间已显示为2.4到7.2秒。燃烧丝释放机构在组件和系统级测试中具有400次点火,没有任何故障。该机制已通过TEPCE(系绳电动推进立方体卫星实验)计划的飞行资格,可以释放两个木匠胶带部署以及一个夹具和系绳部署系统。

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