| 摘要 |
The system comprises a burner-housing in which to ignite volatile fluids, together with means for admitting such fluids thereinto and means for discharging the combustion product therefrom. A coolant-carrying shell is enclosed within the burner-housing, the same having spray holes for discharging coolant onto the burner-housing inner surface, and for discharging coolant into a burner-housing defined combustion chamber. A distributor carried by the shell admits discrete fluids into the housing, and also has coolant passages formed therein. Additionally, the distributor has a fluid-heating arrangement disposed therewithin, as well as a fluid-ignition arrangement, the latter being selectively operative - to insure ignition of the housing-admitted volatile fluids. The combustion products are either simply vented from the burner-housing, for use thus, or are conducted through a terminal rocket nozzle for generating thrust.
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