Development of A Cold Gas Thruster Propulsion TestFor the De-Spin of A Sounding Rocket Recovery System
碩士 === 國立中央大學 === 光機電工程研究所 === 100 === A cold gas thruster propulsion test bed is developed for the de-spin experiment of a sounding rocket recovery system RS of the Sounding Rocket 8 Project. The cold gas thruster propulsion system consists of the pneumatic test bed and the electronic control syste...
| Main Authors: | , |
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| Other Authors: | |
| Format: | Others |
| Language: | zh-TW |
| Published: |
2012
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| Online Access: | http://ndltd.ncl.edu.tw/handle/47460910740993167516 |