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...

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Bibliographic Details
Main Authors: Yao Chia-Hsing, 姚嘉信
Other Authors: 袁曉峰
Format: Others
Language:zh-TW
Published: 2000
Online Access:http://ndltd.ncl.edu.tw/handle/71257213337300894845