ROCKET ENGINE

ROCKET ENGINE

The invention relates to a rocket engine (10) having a thrust chamber (12) bounded by a casing construction (18) with a chamber longitudinal axis (A), wherein the casing construction (18) includes at least one cooling channel (20) in fluidic connection with a source (19) of a cooling medium, wherein...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser: IVANCIC, Blazenko, RIEDMANN, Hendrik, BEHR, Roland, WIEDMANN, Dietmar
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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Beschreibung
Zusammenfassung:The invention relates to a rocket engine (10) having a thrust chamber (12) bounded by a casing construction (18) with a chamber longitudinal axis (A), wherein the casing construction (18) includes at least one cooling channel (20) in fluidic connection with a source (19) of a cooling medium, wherein the cooling channel is traversed by a plurality of bridge elements around which the cooling medium flows and which each extend only over a part, in particular a minor part, of the length of the cooling channel measured along the chamber longitudinal axis (A), and which connect two casing wall pieces (21, 23), bounding the cooling channel on the inside and on the outside of the casing construction, to one another.