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Magnetic fusion engine

Research output: Chapter in Book/Report/Conference proceedingConference contribution

Abstract

A new concept for interplanetary and interstellar missions is discussed. Based on a compact spherical tokamak fusion reactor, this concept can potentially revolutionize human space nights by providing safe and affordable in-space transportation. The goal of this paper is an assessment of the concept employing the recent advances in fusion research. This concept, in contrast to other fusion concepts, utilizes the natural drift motion of charged particles in order to create a directed flux of energetic particles. The momentum of either energetic positive particles or fusion neutrons can be used either directly for propulsion or to heat the hydrogen propellant. One-way trip times are expected to be on a short time scale, such as one to three months for the trip to Mars. Both the exhaust velocity and thrust of the engine may be modulated. This permits the engine to be optimized for a wide variety of missions.

Original languageEnglish (US)
Title of host publicationCollection of Technical Papers - 43rd AIAA/ASME/SAE/ASEE Joint Propulsion Conference
PublisherAmerican Institute of Aeronautics and Astronautics Inc.
Pages5880-5899
Number of pages20
ISBN (Print)1563479036, 9781563479038
DOIs
StatePublished - 2007
Event43rd AIAA/ASME/SAE/ASEE Joint Propulsion Conference - Cincinnati, OH, United States
Duration: Jul 8 2007Jul 11 2007

Publication series

NameCollection of Technical Papers - 43rd AIAA/ASME/SAE/ASEE Joint Propulsion Conference
Volume6

Other

Other43rd AIAA/ASME/SAE/ASEE Joint Propulsion Conference
Country/TerritoryUnited States
CityCincinnati, OH
Period7/8/077/11/07

All Science Journal Classification (ASJC) codes

  • Space and Planetary Science

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