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Merry-go-round-missile mishap

机译:旋转木马导弹事故

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摘要

Early in my career, I was the only engineer responsible for some missile-subassembly test equipment. I knew the system to some extent because I had written the test software, but I lacked the much-needed hardware-troubleshooting experience. I trusted myself on debugging and fixing any software issues, but what now seems like a small test station to me seemed back then like a black hole. I had to fix a problem that had caused multiple UUTs (units under test) to fail the missile's safety-arming tests. The hardware comprised a custom-built test cabin; a VXI chassis and its cabling, both of which we had adopted from another project; and a third-party-supplied centrifuge chamber. We used the centrifuge to simulate a missile launch and test the missile's ability to arm just after traveling some distance. Rotating the centrifuge for 3 to 4 seconds was supposed to cause the application of g force onto an accelerometer in the UUT, in turn causing the missile to arm. For some reason, though, it failed to do so.
机译:在我职业生涯的早期,我是唯一负责一些导弹组件测试设备的工程师。我在某种程度上了解这个系统,因为我编写了测试软件,但我缺乏急需的硬件故障排除经验。我相信自己可以调试和修复任何软件问题,但现在对我来说似乎是一个小型测试站,当时似乎就像一个黑洞。我必须解决一个问题,该问题导致多个UUT(被测单位)无法通过导弹的安全武装测试。硬件包括一个定制的测试舱;VXI底盘及其布线,两者都是从另一个项目中采用的;以及第三方提供的离心室。我们使用离心机模拟导弹发射,并测试导弹在飞行一段距离后的能力。旋转离心机 3 到 4 秒应该会导致 g 力施加到 UUT 中的加速度计上,进而导致导弹武装。然而,由于某种原因,它未能这样做。

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