Numerical Simulation of Monopropellant Hydrazine Thruster

碩士 === 國立成功大學 === 航空太空工程學系碩博士班 === 94 ===   Monopropellant hydrazine thruster has been widely used as the low-thrust power source for attitude control and on-orbit maneuvering of satellites. However, most related studies published in the open literature are mainly experimental. Little has been repor...

Full description

Bibliographic Details
Main Authors: Po-Jeng Tsai, 蔡柏崢
Other Authors: Tsang-Leo Jiang
Format: Others
Language:zh-TW
Published: 2006
Online Access:http://ndltd.ncl.edu.tw/handle/70847448229517541039