发明授权
US08424438B2 Multi-stage rocket, deployable raceway harness assembly and methods for controlling stages thereof
有权
多级火箭,可部署的滚道线束组件及其控制阶段的方法
- 专利标题: Multi-stage rocket, deployable raceway harness assembly and methods for controlling stages thereof
- 专利标题(中): 多级火箭,可部署的滚道线束组件及其控制阶段的方法
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申请号: US12958524申请日: 2010-12-02
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公开(公告)号: US08424438B2公开(公告)日: 2013-04-23
- 发明人: Andrew B. Facciano , Sandie Y. Worley , Robert D. Travis , Dale O. Widmer
- 申请人: Andrew B. Facciano , Sandie Y. Worley , Robert D. Travis , Dale O. Widmer
- 申请人地址: US MA Waltham
- 专利权人: Raytheon Company
- 当前专利权人: Raytheon Company
- 当前专利权人地址: US MA Waltham
- 代理机构: Schwegman Lundberg & Woessner, P.A.
- 主分类号: F41F3/04
- IPC分类号: F41F3/04 ; H02G3/04
摘要:
A deployable raceway harness assembly for use with a multi-stage rocket includes a first cable bundle configured to extend across a second stage of a multi-stage rocket from a guidance unit to a first stage of the rocket. The deployable raceway harness assembly includes a deployable raceway cover configured for detachable coupling with the multi-stage rocket. The deployable raceway cover extends over at least the first cable bundle and a second cable bundle. The first cable bundle is fastened to the deployable raceway cover. The second cable bundle is configured to extend from the guidance unit to the second stage and is shorter than the first cable bundle. An in-flight deployment mechanism is configured to detach the deployable raceway cover and the first cable bundle extending across the second stage from the multi-stage rocket in-flight leaving the second cable bundle extending to the second stage in place.
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