FIELD: space rocket engineering. SUBSTANCE: jet engine has combustion chamber 1, admission nozzle 2, propulsive jet nozzle 3, and combustion products swirler that has tangentially shaped channel 4 and annular chamber 5; swirler communicates through annular channel 6 with outlet propulsive jet nozzle 3. EFFECT: improved design. 10 cl, 14 dwg
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