Ignition anode, in particular for reignitable rocket combustion chambers
An ignition anode for an ignition device of a reignitable rocket combustion chamber. The anode includes an ignition anode body having an ignition anode frontal area. The ignition anode frontal area has a plurality of edges.
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Format: | Patent |
Sprache: | eng |
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Zusammenfassung: | An ignition anode for an ignition device of a reignitable rocket combustion chamber. The anode includes an ignition anode body having an ignition anode frontal area. The ignition anode frontal area has a plurality of edges. |
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