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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Bibliographische Detailangaben
1. Verfasser: Unrath, Dieter
Format: Patent
Sprache:eng
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Beschreibung
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.