The Auto-docking and Auto-separating Mechanism Designed for the Rocket Fuel Loading
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Graphical Abstract
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Abstract
To improve reliability and security of the fueling system in rocket launch, an auto-docking and auto-separating mechanism is designed for the rocket fuel loading. The ADAMS is used to carry out the kinematics and dynamics simulations, getting the connector simulation output curves from the given input ones. The reasonableness and practicality of the designed mechanism are verified by analysis.
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