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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
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
Industrial Applicability	Satellite launch vehicleIn-space propulsion system
Keyword	Direct-Drive Thrust Vector Control Technology Rocket Engine Hybrid Rocket H2O2 Engine Thrust vectoring Direct-Drive Motor Thrust Control Attitude Control