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A Novel Data System for Verification of Internal Parameters of Motor Design

机译:用于验证电机设计内部参数的新型数据系统

摘要

Three major obstacles have limited the amount of information that can be obtained from inside an operating solid rocket motor. The first is a safety issue due to the presence of live propellant interacting with classical, electrical instrumentation. The second is a pressure vessel feed through risk arising from bringing a large number of wires through the rocket motor wall safely. The third is an attachment/protection issue associated with connecting gages to live propellant. Thiokol has developed a highly miniaturized, networked, electrically isolated data system that has safely delivered information from classical, electrical instrumentation (even on the burning propellant surface) to the outside world. This system requires only four wires to deliver 80 channels of data at 2300 samples/second/channel. The feed through leak path risk is massively reduced from the current situation where each gage requires at least three pressure vessel wire penetrations. The external electrical isolation of the system is better than that of the propellant itself. This paper describes the new system.
机译:三个主要障碍限制了可从运行中的固体火箭发动机内部获取的信息量。首先是安全问题,这是由于存在带电的推进剂与经典的电子仪器相互作用。第二个是压力容器穿通的危险,该危险是由于大量导线安全通过火箭发动机壁而引起的。第三是与量具与带电推进剂的连接有关的附着/保护问题。 Thiokol已开发出高度小型化的网络化电气隔离数据系统,该系统已将信息从经典的电气仪表(甚至在燃烧的推进剂表面)安全地传递到外界。该系统仅需四根电线即可以2300个样本/秒/通道的速度传送80个通道的数据。与当前的情况相比,大大降低了穿通泄漏路径的风险,在这种情况下,每个压力计至少需要穿透三个压力容器导线。系统的外部电气隔离性比推进剂本身更好。本文介绍了新系统。

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