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Parametric Optimization of Inductive...

Shimazu, Akihisa.

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Parametric Optimization of Inductively Driven Liner Compression Driver System.

Record Type:	Electronic resources : Monograph/item
Title/Author:	Parametric Optimization of Inductively Driven Liner Compression Driver System./
Author:	Shimazu, Akihisa.
Description:	116 p.
Notes:	Source: Masters Abstracts International, Volume: 55-05.
Contained By:	Masters Abstracts International55-05(E).
Subject:	Aerospace engineering. -
Online resource:	http://pqdd.sinica.edu.tw/twdaoapp/servlet/advanced?query=10138517
ISBN:	9781339940748

Parametric Optimization of Inductively Driven Liner Compression Driver System.
Shimazu, Akihisa.

Parametric Optimization of Inductively Driven Liner Compression Driver System. - 116 p.

Source: Masters Abstracts International, Volume: 55-05.

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

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.

ISBN: 9781339940748Subjects--Topical Terms:

1002622
Aerospace engineering.

Parametric Optimization of Inductively Driven Liner Compression Driver System.
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020 $a 9781339940748
035 $a (MiAaPQ)AAI10138517
035 $a AAI10138517
040 $a MiAaPQ $c MiAaPQ
100 1 $a Shimazu, Akihisa. $3 3192820
245 1 0 $a Parametric Optimization of Inductively Driven Liner Compression Driver System.
300 $a 116 p.
500 $a Source: Masters Abstracts International, Volume: 55-05.
500 $a Adviser: John T. Slough.
502 $a Thesis (Master's)--University of Washington, 2016.
520 $a 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.
590 $a School code: 0250.
650 4 $a Aerospace engineering. $3 1002622
650 4 $a Electromagnetics. $3 3173223
650 4 $a Plasma physics. $3 3175417
690 $a 0538
690 $a 0607
690 $a 0759
710 2 $a University of Washington. $b Aeronautics and Astronautics. $3 2093881
773 0 $t Masters Abstracts International $g 55-05(E).
790 $a 0250
791 $a Master's
792 $a 2016
793 $a English
856 4 0 $u http://pqdd.sinica.edu.tw/twdaoapp/servlet/advanced?query=10138517