The Observation of NTO/MMH Simulants Impinging In High Ambient Pressure
碩士 === 國立成功大學 === 航空太空工程學系碩博士班 === 97 === NTO/MMH thruster has been commonly adopted in spacecraft’s attitude and altitude control because of its high specific impulse (>285sec) and relatively simple system design for the hypergolic characteristics of the propellants. This research utilized the...
| Main Authors: | , |
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| Other Authors: | |
| Format: | Others |
| Language: | zh-TW |
| Published: |
2009
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| Online Access: | http://ndltd.ncl.edu.tw/handle/45492868008972779690 |