Toroidal Spark Gap Engine Tests: Difference between revisions
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| published = 1994 | | published = 1994 | ||
| journal = [[Electric Spacecraft Journal]] | | journal = [[Electric Spacecraft Journal]] | ||
| number = | | number = 11 | ||
| pages = 26-29 | | pages = 26-29 | ||
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Latest revision as of 09:33, 21 July 2026
| Scientific Paper | |
|---|---|
| Title | Toroidal Spark Gap Engine Tests |
| Author(s) | James E Cox |
| Keywords | electrodynamic pulse, high-voltage discharge, plasma generation, toroidal spark gap engine |
| Published | 1994 |
| Journal | Electric Spacecraft Journal |
| Number | 11 |
| Pages | 26-29 |
Abstract
James E. Cox tested and videotaped the forces generated by his six-gap toroidal spark engine. He found it created a short-lived, high-pressure plasma pulse capable of producing dramatic effects. This is a continuation of his work which was presented in ESJ 5 (?Toroidal Spark Gap Engine,? pp. 6-10).