FIELD: production methods; rocket technique.
SUBSTANCE: method includes producing the hole of nozzle and additional processing of its input part by making reciprocal and rotational motion by spike. At the same it is used the spike made of grained pyramid-shaped elaborating surface.
EFFECT: it is provided the stabilization of hydraulic characteristics of nozzle.
4 cl, 3 dwg
Title | Year | Author | Number |
---|---|---|---|
METHOD OF MANUFACTURE OF SPRAY INJECTOR | 1995 |
|
RU2117177C1 |
METHOD OF ELECTROCHEMICAL TREATMENT OF COAXIAL-SPRAY ATOMISER CHANNELS FOR CHAMBER OF LIQUID-FUEL ROCKET ENGINE | 2013 |
|
RU2560892C2 |
PROCESS OF FINISHING OF INJECTORS | 1999 |
|
RU2162394C1 |
ELECTROCHEMICAL TREATMENT METHOD FOR NOZZLE OPENINGS MADE OF CONDUCTIVE MATERIAL | 2013 |
|
RU2550439C2 |
ELECTROCHEMICAL PROCESSING OF NOZZLE ORIFICES | 2013 |
|
RU2556182C2 |
ELECTROCHEMICAL TREATMENT METHOD FOR NOZZLE HOLES | 2013 |
|
RU2543572C2 |
ELECTROCHEMICAL TREATMENT METHOD FOR NOZZLE HOLES | 2013 |
|
RU2557185C2 |
METHOD FOR MAKING JET FORMING NOZZLES | 2012 |
|
RU2579598C2 |
MIXING HEAD OF LIQUID-PROPELLANT ENGINE CHAMBER | 2012 |
|
RU2481491C1 |
METHOD FOR SUPPLYING FUEL COMPONENTS TO LIQUID-PROPELLANT ENGINE CHAMBER | 2012 |
|
RU2481492C1 |
Authors
Dates
2008-05-10—Published
2005-02-07—Filed