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

System and method for manually safing and deorbiting a geostationary spacecraft in an absence of a spacecraft processor
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.
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