FIELD: engines and pumps.
SUBSTANCE: invention relates to aerospace engineering. Proposed plasma engine comprises magnetic core with its central outer end face shifted with respect to pair of opposing magnetic poles in opposite direction of working gas flow. Note here that outer end face of aforesaid magnetic core peripheral part is shifted along working gas flow.
EFFECT: improved focusing of accelerated plasma ion flow, higher efficiency and mechanical durability.
10 cl, 1 dwg
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