Rocket propulsion systems and associated methods

Rocket propulsion systems and associated methods are disclosed. A representative system includes a combustion chamber having an inwardly-facing chamber wall enclosing a combustion zone. The chamber has a generally spherical shape and is exposed to the combustion zone. A propellant injector is couple...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser: Holder, Livingston L, McKinney, Bevin C, Hudson, Gary C
Format: Patent
Sprache:eng
Schlagworte:
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