Further feasibility study on a superconducting linear synchronous motor (LSM) rocket launcher system is presented on the basis of dynamic simulations of electric power, efficiency and power factor as well as the ascending motions of the launcher and rocket. The advantages of attractive-mode operation are found from comparison with repulsive-mode operation. It is made clear that the LSM rocket launcher system, of which the long-stator is divided optimally into 60 sections according to launcher speeds, can obtain high efficiency and power factor.
Electromechanical Dynamics Simulations of Superconducting LSM Rocket Launcher System in Attractive-Mode
1996-07-01
Aufsatz (Konferenz)
Keine Angabe
Englisch
British Library Conference Proceedings | 1996
|DYNAMICS SIMULATIONS OF SUPERCONDUCTING LSM ROCKET LAUNCHER SYSTEM
Online Contents | 1993
|Feasibility Study of Superconducting LSM Rocket Launcher System
British Library Conference Proceedings | 1994
|Rocket/launcher structural dynamics
NTRS | 1976
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