Thruster device for driving e.g. spacecraft, has walls porously formed in injection area, which forms injector for injecting fuel into thrust chamber unit space, so that required fuel is injected during operation of device

The device (10) has a thrust chamber unit (12) including multiple walls (38, 40, 42, 44) that limit a thrust chamber unit space (14). The walls are porously formed in an injection area. The injection area forms an injector for injecting fuel into the thrust chamber unit space, so that 50 percent of...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	ORTELT, MARKUS, HAEBERLE, JUERGEN, HALD, HERMANN
Format:	Patent
Sprache:	eng ; ger
Schlagworte:	BLASTING COMBUSTION ENGINES HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS JET-PROPULSION PLANTS LIGHTING MECHANICAL ENGINEERING WEAPONS
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