Injector Design and Test of a Prototype Low-Thrust Hydrazine Thruster
碩士 === 國立成功大學 === 航空太空工程學系 === 87 === This thesis research has completed the design, fabrication and hot firing tests of a 1-lbf-monopropellant hydrazine thrusters. The design of this thruster is based on the experimental data from previous research in this laboratory. This 1-lbf thruster was equipp...
| Main Authors: | , |
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| Format: | Others |
| Language: | zh-TW |
| Published: |
1999
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| Online Access: | http://ndltd.ncl.edu.tw/handle/61197355466888290764 |