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Spacecraft angular momentum stabilization system and method
Spacecraft angular momentum stabilization system and method
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机译:航天器角动量稳定系统和方法
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摘要
An improved system and method of ejecting a spacecraft from a shuttle or orbiter type craft in space includes a momentum wheel on the spacecraft that has a spin axis parallel to the ejection direction, spinning-up this momentum wheel prior to ejection and after ejection de- spinning this wheel whereby the whole spacecraft spins without the need of a spin table on the shuttle or orbiter craft.
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