A thrust vector control test system of large range solid rocket engine utilizing a four-point support piezoelectric dynamometer and a deflected flange structure
Jin Wang, Zongjin Ren, Jing Yu, Xinyang Li, Jialing Wu, Jun Zhang
Topics & Concepts
FlangeSolid-fuel rocketThrustDeflection (physics)DynamometerAerospace engineeringStructural engineeringPiezoelectricityEngineeringRocket engineAcousticsMechanical engineeringMaterials sciencePhysicsPropellantOpticsElectrical engineeringRocket and propulsion systems researchMechatronics Education and ApplicationsAdvanced Measurement and Detection Methods