| 摘要 |
A propulsion motor for rockets and spaceships comprising two cylindrical rings ( 17 ) linked by means of a bar ( 18 ) forming the motor external structure ( 17,18 ) and an exhaust ( 13,14,15 ) linked to a third cylindrical ring ( 17 A) and to a reactor room ( 16 ) where nuclear fuel ( 3 ) explodes and generates a beam ( 8 ) directed to another nuclear fuel ( 10 ) inside the exhaust ( 13,14,15 ) which produces a thrust to a reflector magnetic field ( 12 ) and the hot plasma avoids touching the exhaust wall ( 13 ). To initiate reactions in the reactor vessel ( 6 ) and in the exhaust ( 13,14,15 ) an injection system ( 19 ) and a production system ( 20 ) the fuel ( 3,10 ) are needed.
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