| Technical Name | Modularized and Throttleable Hydrogen Peroxide Hybrid Rocket Engine with Direct-Drive Thrust Vector Control Technology | ||
|---|---|---|---|
| Project Operator | National Chiao Tung University | ||
| Project Host | 吳宗信 | ||
| Summary | Modularized and Throttleable Hydrogen Peroxide Hybrid Rocket Engine with Direct-Drive Thrust Vector Control Technology |
||
| Scientific Breakthrough | We use liquid hydrogen peroxide water as oxidants and solid plastics as fuel for hybrid rocket engines. The characteristic of combustion is like candles, which is safe, easy to save and not prone to explosion.Around 90% of the injection flow of hydrogen peroxide water are used to control the engine thrust which is a simple and low cost system that the engine vacuum specific impulse is over 300 seconds. |
||
| Industrial Applicability | Satellite launch vehicle and In-space propulsion system |
||
| 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 | ||
| Notes | |||
- Contact
- tiaopidaoda@gmail.com
other people also saw