DETONATION ROCKET ENGINE

DETONATION ROCKET ENGINE

Detonation rocket engine comprising an aerospike nozzle (4), an annular detonation chamber (5) connected to the aerospike nozzle (4), and lines (2, 3) for supplying propellant components connected to the detonation chamber (5). The detonation chamber (5) has a bottom (9) connecting an inner wall (10...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser: Wola ski, Piotr, Kawalec, Micha
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:Detonation rocket engine comprising an aerospike nozzle (4), an annular detonation chamber (5) connected to the aerospike nozzle (4), and lines (2, 3) for supplying propellant components connected to the detonation chamber (5). The detonation chamber (5) has a bottom (9) connecting an inner wall (10) and an outer wall (11) between which an outlet (6) is formed. At the outlet (6) of the detonation chamber (5) there are at least three evenly distributed centring elements (1) connecting the inner wall (10) and the outer wall (11) of the detonation chamber (5), with cooling channels (7) connected to one of the lines (2, 3) supplying the propellant components to the detonation chamber (5).