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Linear Electric Motors for Aerospace Launch Assist
This paper summarizes the results of a design study investigating the use of linear electric motors in an aerospace electromagnetic launcher application requiring 7g's of horizontal acceleration to a velocity of 300mls. ...
The Conceptual Design of a Lightweight Compulsator-Driven Electromagnetic Accelerator
The development of light-weight pulsed power supplies which can deliver significant amounts of energy in a properly conditioned pulse has been an issue throughout the investigation of electromagnetic (EM) launchers and ...