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Missile test method for testing the operability of a missile from a launch site

机译:用于从发射场测试导弹可操作性的导弹测试方法

摘要

A missile is tested by first stimulating the performance of missile built-in tests that are stimulated in service by signals from the launch site, and which tests do not require internal access to the missile. If performance is satisfactory, no further testing is required. If a condition of unsatisfactory missile performance is detected, an access cover is removed, connections are made to internal sources of data, and the built-in tests are repeated in order to determine which internal components caused the unsatisfactory missile performance. The component is repaired. The testing with the access cover removed is repeated, and, if the performance is satisfactory, the access cover is replaced and the testing with the access cover present is repeated.
机译:首先通过刺激导弹内置测试的性能来测试导弹,该内置测试在发射场的信号的作用下被激发,并且这些测试不需要内部进入导弹。如果性能令人满意,则无需进一步测试。如果检测到导弹性能不理想的情况,则拆下检修盖,与内部数据源建立连接,并重复进行内置测试,以确定哪些内部组件导致了导弹性能不理想。组件已修复。重复进行拆下检修盖的测试,如果性能令人满意,则更换检修盖,并在存在检修盖的情况下重复进行测试。

著录项

  • 公开/公告号US5721680A

    专利类型

  • 公开/公告日1998-02-24

    原文格式PDF

  • 申请/专利权人 HUGHES MISSILE SYSTEMS COMPANY;

    申请/专利号US19950478148

  • 发明设计人 DAVID P. VAN CLEVE;R. WINSTON MONK;

    申请日1995-06-07

  • 分类号G06F15/14;F41G7/00;

  • 国家 US

  • 入库时间 2022-08-22 02:40:09

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