Samtec SEAM和SEAF连接器在空间应用中用作印刷电路板组装(PCBA)堆叠连接器的资格认证

Neil Dalal, Nabid Farvez, Kyle Anderson, Allison M. Orr, S. Ling, R. Hacala
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引用次数: 0

摘要

在过去的太空任务中,约翰霍普金斯大学应用物理实验室(JHU/APL)的模块化电子设计利用了通孔IEH Hypertronics堆叠连接器。为了满足即将到来的蜻蜓任务对泰坦的需求,APL寻求更高密度的选择,因为印刷电路板组装(PCBA)空间将是一个主要的限制因素。Samtec SEAM和SEAF连接器被确定为通过完整空间环境测试资格的最佳候选产品。连接器需要将pcb堆叠在一起,具有200+输入/输出(I/O),能够承受振动,冲击和热环境,低放气,并实现大于200mhz的信号完整性。SEAM和SEAF连接器对也很有吸引力,因为它们的表面安装而不是通孔板连接,而且间距小(0.050英寸)。虽然SEAM和SEAF连接器不属于令人担忧的“音叉”类别,但它们没有EEE-INST-02要求的多点接触,因此资格测试是证明空间应用连接器可靠性的唯一方法。完成的测试单元进行环境测试包括两个5“切片”测试“盒”,一个用于240针连接器,一个用于400针连接器。每个切片由SEAM和/或SEAF连接器组成,组装到6.5“x 3.7”x 0.093“印刷电路板(PCB)上,并安装在铝制框架中,连接器周围有加强筋,以最大限度地减少由于振动引起的动态位移。在组装过程中,在将连接器手工放置到PCBA上之前,通过模板和喷射打印将额外的焊料沉积在电路板上。通过x射线和CT扫描证实,这两种方法都成功地将连接器安全地连接到电路板上,没有短路或打开。每个测试箱包含4个SEAM和4个SEAF连接器,因为每个端片只包含一个连接器,从而形成一个闭环菊花链,可以监测四线电阻,以评估连续性和间歇性。通过将每个切片与其相邻的切片配合,然后包括端盖和螺纹杆,组装了5片盒。资格测试遵循APL的“随飞测试”原则。在接线盒组装之前,对切片之间的每个连接器接口进行了20次循环匹配和衰减测试,以确认每个引线镀金的完整性。对原型机GEVS 14.1 gRMS进行了随机振动试验,并在三个轴上进行了2828 g的冲击试验,间歇监测分辨率为50纳秒。随后,在-40°C至+125°C范围内完成了400多次空气热循环,以完成APL最严酷的热循环任务。在测试计划的每一步中,都要进行四线电阻测量,以确认菊花链连接,从而确保堆叠连接器按预期工作。经过严格的环境测试后,采用横截面来评估焊点的完整性,并评估最小损害,以进一步降低风险。SEAM和SEAF连接器将完成连接器组装过程,然后在类似飞行的测试箱上进行全面的资格测试,然后将继续用于空间应用。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Qualification of the Samtec SEAM and SEAF connectors for use as a printed circuit board assembly (PCBA) stacking connector in space applications
The Johns Hopkins University Applied Physics Laboratory’s (JHU/APL) modular electronics design on past space missions leverages the through-hole IEH Hypertronics stacking connector. To meet the needs of the upcoming Dragonfly mission to Titan, APL searched for a higher density option because a major limiting factor will be printed circuit board assembly (PCBA) space. The Samtec SEAM and SEAF connectors were identified as the best candidate to flow through a full space environmental test qualification. The connector needed to stack PCBAs together, have 200+ input/output (I/O), survive vibration, shock, and thermal environments, be low outgassing, and accomplish greater than 200 MHz signal integrity. The SEAM and SEAF connector pair were also attractive because of their surface mount instead of through-hole board attachment as well as small pitch (0.050’’). Although the SEAM and SEAF connectors do not fall under the worrisome ‘tuning fork’ category, they do not have a multi-point contact required by EEE-INST-02 so a qualification test was the only way to prove reliability of the connectors for space application.The completed test units undergoing environmental testing consisted of two 5-"slice" test "boxes", one for 240-pin connectors and one for 400-pin connectors. Each slice consisted of SEAM and/or SEAF connectors assembled to a 6.5’’ x 3.7’’ x 0.093’’ printed circuit board (PCB) and mounted into an aluminum frame with a stiffener surrounding the connector to minimize dynamic displacement due to vibration. Additional solder was deposited on the board during the assembly process via stencil as well as jet printing before the connector was hand placed onto the PCBA. Both methods to complement the solder charged connector leads were successful in securely attaching the connectors to the board without shorts or opens as confirmed by X-ray and CT scanning. Each test box contained four SEAM and four SEAF connectors as each end slice only contained one connector to have a closed-loop daisy chain that could be monitored for four-wire resistance to assess continuity and intermittence. The 5-slice boxes were assembled by mating each slice to its adjacent neighbor one at a time followed by the inclusion of end covers and threaded rods.The qualification test followed APL’s test-as-you-fly principle. Prior to box assembly, a 20-cycle mate and demate test was performed on each connector interface between slices to confirm the integrity of each lead’s gold plating. Random vibration to protoflight GEVS 14.1 gRMS and shock testing to 2828 g’s were conducted in all three axes with intermittence monitoring to 50 nanosecond resolution. Subsequently, 400-plus cycles of in-air thermal cycling from -40 to +125 °C was completed to bound the harshest conceivable thermal cycling mission at APL. Every step of the test plan, a four-wire resistance measurement was taken to confirm the daisy chain connection and consequently that the stacking connectors were functioning as intended. Cross-sectioning was pursued to assess solder joint integrity after the rigorous environmental testing and minimal damage is under assessment for further risk mitigation. By completing a connector assembly process followed by a comprehensive qualification test on flight-like test boxes, the SEAM and SEAF connectors will proceed for use in space applications.
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