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A method for evaluating the thrust of a space propulsion device with wide range time variations using a disturbance observer
Kakami, Akira, Muto, Takuya, Yano, Yasuyuki, Tachibana, TakeshiVolume:
86
Language:
english
Journal:
Review of Scientific Instruments
DOI:
10.1063/1.4935884
Date:
November, 2015
File:
PDF, 1.14 MB
english, 2015