| 摘要 |
Short-duration, high-power-density thruster, in particular for projectiles enclosing a tapered rod acting by kinetic energy alone, this thruster comprising a reserve of liquid propergol with several components which is burned in a combustion chamber 26 equipped with a thrust tube 10 mounted downstream, characterised in that the reserve of liquid propergol is stored in the form of a column of liquid 38 directly in the combustion chamber 26, that the components A, B of the propergol are regularly distributed in one another in the liquid column and are separated by destructible or retractable partitions 34 and that, for fixing the liquid column during combustion, one wall is arranged on the rear end, in the direction of flight, of the combustion chamber. <IMAGE>
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