Parametric Optimization of Inductively Driven Liner Compression Driver System


Autoria(s): Shimazu, Akihisa
Contribuinte(s)

Slough, John T

Data(s)

14/07/2016

14/07/2016

01/06/2016

Resumo

Thesis (Master's)--University of Washington, 2016-06

The performance of an Inductively Driven Liner Compression (IDLC) driver system for the Fusion Driven Rocket (FDR) application is optimized in this study by performing a parametric analysis of the IDLC driver configurations. The FDR is a novel concept developed by MSNW LLC, which directly converts fusion energy into propulsive energy, where the fusion energy is produced by an inductively driven metal liner compression of a Field Reversed Configuration (FRC) plasmoid. To identify the optimum system configuration for the IDLC driver system for the FDR, a 1D liner code is developed in this study to run different test configuration cases and to identify the optimum system configuration. The results from the 1D liner code is verified against a commercial SPICE circuit solver and a commercial explicit structural dynamics code to verify that the 1D liner code correctly captures the essential liner dynamics for performance tuning. The parametric analysis results from the 1D liner code showed that the IDLC driver system prefers higher voltage to capacitance for a fixed capacitor bank energy. A slightly negative initial seed flux is also seen to improve the liner compression performance. For the optimized design point identified in this study, an energy coupling between the liner kinetic energy and the bank capacitive energy of 69 % is obtained for a fixed capacitor bank energy of 1.8 MJ.

Formato

application/pdf

Identificador

Shimazu_washington_0250O_15817.pdf

http://hdl.handle.net/1773/36478

Idioma(s)

en_US

Palavras-Chave #FRC #Imploding liners #Inductive drive #Magneto-inertial fusion #Metal liners #Aerospace engineering #Electromagnetics #Plasma physics #aeronautics and astronautics
Tipo

Thesis