IGNITER FOR A ROCKET ENGINE, METHOD FOR IGNITION OF A ROCKET ENGINE

An igniter for a rocket engine or motor comprising a combustion chamber with a solid fuel, an inlet for supplying an oxidizer to the combustion chamber to ignite the solid fuel and an outlet for discharging exhaust gas, wherein the igniter is arranged to discharge exhaust gas to the rocket engine fo...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	WELLAND-VELTMANS, WILHELMINA HELENA MARIA, VERMEULEN, EDUARDUS JOSEPHUS, BRAUERS, BERND MATHIAS JOZEF
Format:	Patent
Sprache:	eng ; fre
Schlagworte:	BLASTING COMBUSTION ENGINES HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS JET-PROPULSION PLANTS LIGHTING MECHANICAL ENGINEERING WEAPONS
Online-Zugang:	Volltext bestellen
Tags:	Tag hinzufügen Keine Tags, Fügen Sie den ersten Tag hinzu!