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Low Current Surface Flashover Triggering System
Summary
Researchers at Purdue University have developed a triggering system for electric micropropulsion systems. The system incorporates a low current surface flashover and is capable of operating reliably for a large number of triggering events. This device would be used in micropropulsion systems but can be part of an entire micropropulsion system.
Technology Benefits
Low current surface flashoverLong lifespanReliable
Technology Application
Micropropulsion systems
Detailed Technology Description
Alexey ShashurinPurdue Aeronautics and Astronautics
Countries
United States
Application No.
None
Country/Region
USA
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