| Technical Name | Modularized ana Throttleable Hydrogen Peroxide Hybrid Rocket Engine with Direct-Drive Vector Control Technology | ||
|---|---|---|---|
| Project Operator | National Chiao Tung University | ||
| Project Host | 吳宗信 | ||
| Summary | ModularizedThrottleable Hydrogen Peroxide Hybrid Rocket Engine with Direct-Drive Thrust Vector Control Technology |
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| Scientific Breakthrough | We use liquid hydrogen peroxide water as oxidantssolid plastics as fuel for hybrid rocket engines. The characteristic of combustion is like candles, which is safe, easy to savenot prone to explosion. Around 90 of the injection flow of hydrogen peroxide water are used to control the engine thrust which is a simplelow cost system that the engine vacuum specific impulse is over 300 se |
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| Industrial Applicability | Satellite launch vehicleIn-space propulsion system |
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| Keyword | Direct-Drive Thrust Vector Control Technology Rocket Engine Hybrid Rocket H2O2 Engine Thrust vectoring Direct-Drive Motor Thrust Control Attitude Control | ||
| Notes | |||
- Contact
- fthwang@nspo.narl.org.tw
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