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Nuclear physics / Magnetized target fusion / Fusion rocket / Inertial confinement fusion / Nuclear fusion / Lawson criterion / Plasma / Fusion energy gain factor / Beta / Fusion power / Physics / Energy


Nuclear Propulsion based on Inductively Driven Liner Compression of Fusion Plasmoids John Slough1 and David Kirtley
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Document Date: 2012-10-02 00:11:47


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City

Kirtley / Slough / Oxon / D. / Salt Lake City / Dudzinski / Juhasz / Borowski / L.A. / /

Company

3He FRC Isp LC / Robson A.E. / Ryutov D.D. / /

Continent

America / /

Country

United Kingdom / /

Facility

American Institute of Aeronautics / David Kirtley University of Washington / University of Washington / FRC facility / /

IndustryTerm

approximate analytical solution / chemical rockets / space travel / rapid planetary travel / radiation energy / axial magnetic field energy / heated gas rocket / launch propulsion systems / kJ bank / rapid manned space travel / fusion energy production / fusion neutron energy / fusion energy / high energy density / in-space transportation / planetary travel / energy density / liner thermal energy / higher energy yield / liner kinetic energy / inspace transportation / thermal energy / gas giants / energy confinement / high energy density regime / electric energy / magnetic energy / energy / remnant liner thermal energy / scale fusion systems / energy density gain / propulsion applications / electricity / energy techniques / fusion particle energy / metal liners / rapid manned interplanetary space travel / gas temperatures / capacitor bank / metal liner fusion / kinetic energy / directed propulsive energy flow / fusion products / large kinetic energy / large specific energy / electrical energy / fission energy / space propulsion applications / thin metal liner / metal liner / propulsion technology / chemical combustion / fusion plasma energy loss / large energy yield / chemical engine / directed energy / chemical combustion energy / energy efficiency / charged particle fusion products / optimized compression bank / energy release / space transportation / metal rings / fusion energy yields / power systems / chemical rocket / chemical propulsion gas temperatures / liner radial implosion kinetic energy / /

MusicGroup

UT / /

Organization

Department of Energy / Department of Aeronautics and Astronautics / American Institute of Aeronautics and Astronautics / American Institute of Aeronautics and Astronautics References / office of Fusion Energy Sciences / University of Washington / Seattle / /

Person

Cnare / Al vmax / /

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Position

Driver / good conductor / Acknowledgments The author / /

Product

America / /

ProvinceOrState

S.K. / Washington / Utah / S. K. / /

PublishedMedium

Journal of Applied Physics / /

Technology

radiation / Fusion Technology / heat transfer / lasers / condensation / ISP / existing propulsion technology / /

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