A Study of The Start Up Delay for Low-Thrust Hydrazine Thrusters
碩士 === 國立成功大學 === 航空太空工程學系 === 88 === Abstract This thesis research has completed the design, fabrication and hot firing tests of a 1-lbf-monopropellant hydrazine thrusters. The design of this thruster was based on the experimental data from previous researches of this laborato...
Main Authors: | , |
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Other Authors: | |
Format: | Others |
Language: | zh-TW |
Published: |
2000
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Online Access: | http://ndltd.ncl.edu.tw/handle/71257213337300894845 |