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The YF-40 is a Chinese liquid rocket engine burning N2O4 and UDMH in an gas generator cycle. It has dual gimbaling combustion chambers. Originally it was developed for the Long March 1D second stage.〔 It is used on the third stage of the Long March 4 family of launch vehicles.〔〔〔 ==References== 抄文引用元・出典: フリー百科事典『 ウィキペディア(Wikipedia)』 ■ウィキペディアで「YF-40」の詳細全文を読む スポンサード リンク
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