Invention Grant
US09346564B1 System and method for manually safing and deorbiting a geostationary spacecraft in an absence of a spacecraft processor
有权
在没有航天器处理器的情况下手动安装和去除对地静止航天器的系统和方法
- Patent Title: System and method for manually safing and deorbiting a geostationary spacecraft in an absence of a spacecraft processor
- Patent Title (中): 在没有航天器处理器的情况下手动安装和去除对地静止航天器的系统和方法
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Application No.: US13898421Application Date: 2013-05-20
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Publication No.: US09346564B1Publication Date: 2016-05-24
- Inventor: Kurt M. Rump , Richard A. Noyola , Steven E. Ardito , Adriel O. Carreno
- Applicant: The Boeing Company
- Applicant Address: US IL Chicago
- Assignee: The Boeing Company
- Current Assignee: The Boeing Company
- Current Assignee Address: US IL Chicago
- Agency: McDonnell Boehnen Hulbert & Berghoff LLP
- Main IPC: B64G1/10
- IPC: B64G1/10 ; B64G1/24

Abstract:
A system and method for controlling de-orbit of a spacecraft is presented. Embedded command modules are commanded directly from a central command and telemetry module. Latch valves, thruster valves, and solar wing drive of the spacecraft are operated in response to inputs to the embedded command modules. The spacecraft is maneuvered to a safe disposal orbit in response to commands from the central command and telemetry unit.
Information query