Design and Analysis of a Fuel Tank for a Satellite Attitude-Control System
碩士 === 國立成功大學 === 航空太空工程學系碩博士班 === 101 === The purpose of this thesis is to develop a propellant fuel tank which can be applied to space environment. The design of this fuel tank is mainly divided into two major structural parts which are cylindrical fuel tank and internal piston/seal accessory. The...
| Main Authors: | , |
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| Other Authors: | |
| Format: | Others |
| Language: | zh-TW |
| Published: |
2013
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| Online Access: | http://ndltd.ncl.edu.tw/handle/96438144570207549862 |