Toroidal Spark Gap Engine: Difference between revisions
Appearance
Imported from text file |
infobox: unlink bare volume/issue numbers (removes redlinks to numeric titles) |
||
| Line 5: | Line 5: | ||
| published = 1992 | | published = 1992 | ||
| journal = [[Electric Spacecraft Journal]] | | journal = [[Electric Spacecraft Journal]] | ||
| number = | | number = 5 | ||
| pages = 6-10 | | pages = 6-10 | ||
}} | }} | ||
Latest revision as of 09:33, 21 July 2026
| Scientific Paper | |
|---|---|
| Title | Toroidal Spark Gap Engine |
| Author(s) | James E Cox |
| Keywords | do-it-yourself, launching device, toroidal spark gap engine |
| Published | 1992 |
| Journal | Electric Spacecraft Journal |
| Number | 5 |
| Pages | 6-10 |
Abstract
Large electromagnetic thrusts in air can be obtained from the discharge of advanced capacitors into a toroidal spark gap engine (TSGE). Details of how to build a small model are presented. A fully-developed, air-breathing TSGE pulse-jet could launch a small delta wing vehicle into earth orbit, powered from a concentrated solar beam generator located and operating already in Barstow, California. Many technical issues must be addressed, such as thermal management, the existence of waste solar heat on the vehicle, and improving engine performance.