Spin stability is taken for the small lunar explorer to build up the solid m otor firing attitude when it was injected from the Earth-berth orbit to the Ear t h-Moon transfer orbit.

 
  • 小型月球探測器由地球停泊軌道向地月轉移軌道射入時(shí),要求采用自旋穩定來(lái)建立發(fā)動(dòng)機的點(diǎn)火姿態(tài)。
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