| Technical Name | ModularizedThrottleable Hydrogen Peroxide Hybrid Rocket Engine with Direct-Drive Thrust Vector Control Technology | ||
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| Project Operator | 吳宗信 | ||
| 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 sec |
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| Industrial Applicability | Satellite launch vehicleIn-space propulsion system |
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| Keyword | Hybrid Rocket Engine Thrust Vector Control Trajectory control 3D Metal Printing Modularized Direct-Drive Motor Throttle Control H2O2 Engine system N2O Engine system Composite Material | ||
- tiaopidaoda@gmail.com
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