Compact, high performance swirl combustion rocket engine

A compact rocket engine with advanced swirl combustion can generate vacuum thrust in the 500 1b f to 100,000 1b f range. The rocket engine (10) includes a feed system (21), combustor assembly (12), swirl generator (14) and nozzle (16). The feed system (21) delivers the oxidizer and fuel (18,20) to t...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	SCHMOTOLOCHA, STEPHEN N, PEDERSON, ROBERT J
Format:	Patent
Sprache:	eng ; fre ; ger
Schlagworte:	BLASTING COMBUSTION ENGINES HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS JET-PROPULSION PLANTS LIGHTING MECHANICAL ENGINEERING WEAPONS
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