日本航空宇宙学会論文集
Online ISSN : 2432-3691
Print ISSN : 1344-6460
ISSN-L : 1344-6460
論文
低電力電気推進用の微小推力測定スタンド
小泉 宏之各務 聡小紫 公也荒川 義博
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ジャーナル フリー

2003 年 51 巻 593 号 p. 270-275

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A torsional-type thrust stand has been designed in order to measure precisely the impulse bits produced by low-power pulsed plasma thrusters. The stand is capable of measuring impulse bits ranging from 10 to 1,000 μNs in vacuum conditions. Investigations concerning extremely low impulse measurement have encountered difficulties in the past due to undesired vibrations of the measuring facility. The relation between the background noise and the excited vibrations to the thrust stand is considered and it is shown that an optimum damping ratio exists which provides a maximum SN (signal-to-noise) ratio.

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© 2003 The Japan Society for Aeronautical and Space Sciences
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