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  • Launch Vehicles and Launch Operations  (1)
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    Publication Date: 2019-07-13
    Description: The slingatron mass accelerator is described for several track configurations (shapes), and numerical simulations of this accelerating mass traversing a given track configuration are presented. The sled is modeled as a point mass that interacts with the slingatron track using both a conventional and a new empirical velocity dependent friction law. The closed loop circular slingatron was found to produce high maximum sled velocities provided the gyration angular speed is always increasing. In contrast several spiral shaped slingatron tracks reveal that high maximum sled velocities are obtainable with the gyration speed held constant. In fact, a slingatron constructed out of semi-circles is shown capable of generating high velocity sleds in such a way that no initial sled injection is necessary. Choosing the proper initial gyration phase with an empirically determined friction model allows the mass sled to gain ever-increasing velocities when placed in a semi-circle slingatron. The sled bearing pressure and its total acceleration are examined and presented.
    Keywords: Launch Vehicles and Launch Operations
    Type: ARL-RP-30 , Proceedings of the 10th US Army Gun Dynamics Symposium|10th US Army Gun Dynamics Symposium; Apr 23, 2001 - Apr 26, 2001; Austin, TX; United States
    Format: text
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