FIELD: rocketry; production of the charges made out of the mixed solid rocket fuels.
SUBSTANCE: the invention is pertaining to the production of the charges made out of the mixed solid rocket fuels, in particular, to liquidation of the charges made out of the MSRF in the housings of the rocket engines, mainly of the channel-type rocket engines. The composition contains water, polyacrylamide, the powdery anionic polyacrylamide with thee degree of hydrolysis of 10-50 mole %, the molecular mass - up to 14-106, the size of particles - 750-1500 microns and the inorganic salts - potassium bichromate, sodium thiosulfate. The technical result of the invention is simplification of the technological process of preparation of the flegmatizing refrigerant, reduction of the solidification time of the flegmatizing refrigerant composition.
EFFECT: the invention ensures simplification of the technological process of preparation of the flegmatizing refrigerant, reduction of the solidification time of the flegmatizing refrigerant composition.
2 tbl
Title | Year | Author | Number |
---|---|---|---|
METHOD FOR PRODUCTION OF PHLEGMATIZING COMPOUND FOR LIQUIDATION OF MIXED SOLID-PROPELLANT CHARGES | 2005 |
|
RU2284012C1 |
COMPOSITION OF PHLEGMATICAL COOLING AGENT FOR CONTROLLED RETARDED BURNING OUT OF SOLID ROCKET FUEL CHARGES, SOLID ROCKET FUEL WASTE, AND EXPLOSIVES | 1997 |
|
RU2145330C1 |
METHOD FOR DESTRUCTION OF CHARGES OF SOLID PROPELLANT | 2003 |
|
RU2245511C1 |
PHLEGMATIZING COOLING AGENT COMPOSITION FOR CONTROLLED DELAYED COMBUSTION OF SOLID ROCKET FUEL CHARGES, SOLID ROCKET FUEL WASTE, AND EXPLOSIVES | 2003 |
|
RU2261238C1 |
METHOD FOR DESTRUCTION OF SOLID PROPELLANT CHARGES, WASTE OF SOLID PROPELLANT AND EXPLOSIVES BY REGULATED SLOWED DOWN INCINERATION WITH THE USE OF PHLEGMATIZING COOLANT | 2005 |
|
RU2300731C2 |
MOVABLE PLANT FOR PREPARING AND SUPPLYING RETARDING COMPOSITION TO SPACES IN CHARGES OF SOLID ROCKET ENGINES | 2005 |
|
RU2288205C1 |
METHOD FOR ELIMINATION OF CHARGE OF LARGE-SIZED SOLID-PROPELLANT ROCKET ENGINE WITHOUT NOZZLE UNIT BY COMBUSTION METHOD | 2005 |
|
RU2301959C2 |
METHOD OF DESTRUCTION OF SOLID-PROPELLANT CHARGES | 1997 |
|
RU2133410C1 |
METHOD OF DESTRUCTION OF SOLID PROPELLANT CHARGES | 1997 |
|
RU2123991C1 |
EPOXIDE MOULDING COMPOSITION FOR ARMOR PLATING SET-IN GRAIN OF COMPOSITE SOLID PROPELLANT | 2007 |
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RU2330832C1 |
Authors
Dates
2006-05-27—Published
2005-05-20—Filed