FIELD: rocket engineering. SUBSTANCE: proposed chamber contains combustion chamber with nozzle and mixing head. Mixing head consists of housing, pack of plates with feed channels in form of through holes in some plates and injector channels in said adjacent plates communicating with corresponding manifolds, all being installed in housing. Pack is made up of ring plates with radial injector channels. EFFECT: simplified design process of manufacture of chamber for liquid-propellant low-thrust engine. 3 cl, 6 dwg
| Title | Year | Author | Number |
|---|---|---|---|
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|
RU2217620C2 |
| INJECTOR ASSEMBLY | 1999 |
|
RU2191913C2 |
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|
RU2288370C2 |
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|
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RU2685166C2 |
