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pro vyhledávání: '"陳秋富"'
Autor:
Chen qui-fu, 陳秋富
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The surface-tension type propellant tank is generally adopted in the baseline design of 500-kg class satellites. For this specific type of propellant tank, there is no diaphragm to physically separate the liquid hydrazine (N2H4) from the pres
The surface-tension type propellant tank is generally adopted in the baseline design of 500-kg class satellites. For this specific type of propellant tank, there is no diaphragm to physically separate the liquid hydrazine (N2H4) from the pres
Externí odkaz:
http://ndltd.ncl.edu.tw/handle/91526356039789032341
