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Propulsion of space ships by nuclear explosion

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Abstract

Recent progress in the research on deuterium-tritium (D-T) inertially confined microexplosions encourages one to reconsider the nuclear propulsion of spaceships based on the concept originally proposed in the Orion project. We discuss first the acceleration of medium-sized spaceships by D-T explosions whose output is in the range of 0.1–10 t of TNT. The launching of such a ship into an Earth orbit or beyond by a large nuclear explosion in an underground cavity is sketched out in the second section of the paper, and finally we consider a hypothetical Mars mission based on these concepts. In the conclusion it is argued that propulsion based on the Orion concept only is not the best method for interplanetary travel owing to the very large number of nuclear explosion required. A combination of a super gun and subsequent rocket propulsion using advanced chemical fuels appears to be the best solution for space flights of the near future.

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Authors and Affiliations

  1. University of Ferrara, via Paradiso 12, 44100, Ferrara, Italy

    J. G. Linhart

  2. Technical University, Prague 6, Technická, Czech Republic

    J. Kravárik

Authors
  1. J. G. Linhart
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  2. J. Kravárik
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From Kosmicheskie Issledovaniya, Vol. 43, No. 1, 2005, pp. 67–75.

Original English Text Copyright © 2005 by Linhart, Kravárik.

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Linhart, J.G., Kravárik, J. Propulsion of space ships by nuclear explosion. Cosmic Res 43, 65–72 (2005). https://doi.org/10.1007/s10604-005-0019-3

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  • DOI: https://doi.org/10.1007/s10604-005-0019-3

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