Rocket control surfaces. The roll angle stabil-isation is realised by auxil...
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Rocket control surfaces. The roll angle stabil-isation is realised by auxiliary surfaces (ailerons). Fins in place at the top of a 70 m-tall Super Heavy Booster 4: Source The booster is used for the SpaceX Starship program. The actuators of the attitude-stabilization system in the longitudinal and lateral motions are four control surfaces (fins) that may rotate in pairs about their axes. 1 Rocket Dynamics We consider a winged rocket that has a canard aerodynamic configuration and is equipped with a solid propellant engine. Abstract This paper presents study of control and the static stability of a rocket plane. The concept of the rocket plane control assumes two types of control surfaces. Roll is a measure of how much the rocket has rotated on its longest axis. These control surfaces would require actuators with microscale features. The actuator system generates 3. The results presented in this paper demonstrate the feasibility of a sufficiently low mass flight controller, paving the way for a small scale rocket system to deliver a 10g attosatellite into low Earth orbit (LEO).
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