The short-circuited grid components are often the factors crucial to the failure of ion rocket propulsion system.

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In this Paper, both theoretical and expenimental investigations about the power distribution and control system of a xenon ion rocket engine are described.

本文從理論和實驗兩個方面對氙離子火箭發(fā)動機配電及控制系統(tǒng)進行了研究色综合色欲色综合色综合色综合，并設計出以8031單片機為核心組成的微機實時監(jiān)控系統(tǒng)。

This article tries to give readers an elementary impression of the interaction of spacecraft and plasma (space plasma and plasma produced by the ion rocket engine) in a simple way, it also gives some advice to those who design spacecraft.

文章試圖以一種較簡明的方式讓讀者對航天器與等離子體（空間等離子體以及發(fā)動機產生的等離子體束流）的相互作用有一個初步的概念99r在线观看视频精品，并對航天器的設計給出幾點建議女性毛片A。

The method of ignition transient interior ballistic calculat ion of solid rocket motor was presented. Many factors influencing the performance of interior ballistic such as e rosive burning,friction,pressure velocity were taken into consideration.

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ion rocket：離子火箭

ion pump 離子泵 | ion rocket 離子火箭 | ion sputter deposition 濺射蒸涂

ion rocket：離子推進火箭

ionosphere beacon satellite 遊離層信標衛(wèi)星 | ion rocket 離子推進火箭 | IR augmenter 紅外線增強器