FIELD: weapons.
SUBSTANCE: invention relates to rocket engineering. The proposed method comprises mixing propellant components up in a neutral medium, squeesing the propellant mass, rolling the said mass along with processing till molded mass, drying the latter and producing from it the charges using forming press. In mixing the aforesaid components in neutral medium, combustion inhibitor, i.e. γ-polyoxymethylene with the mean grain size not exceeding 15.0 μ is added thereto. Note also that and nitrocelluloses is used with nitrogen content not exceeding 192.0 ml NO/g.
EFFECT: propellant combustion rate of 2,2 to 3,85 mm/s at Pk=40 kgf/cm2 and T=20°C.
1 tbl
| Title | Year | Author | Number |
|---|---|---|---|
| MANUFACTURING METHOD OF CHARGE FROM BALLISTIC SOLID PROPELLANT | 2008 |
|
RU2384555C2 |
| METHOD OF PRODUCING CHARGE FROM SOLID BALLISTITE ROCKET PROPELLANT | 2008 |
|
RU2360894C1 |
| METHOD FOR CHARGE MANUFACTURING FROM HIGH-FILLED SOLID BALLISTITE ROCKET FUEL | 2010 |
|
RU2441860C1 |
| METHOD FOR PRODUCTION OF SOLID PROPELLANT CHARGE OF BALLISTITE TYPE | 2008 |
|
RU2378238C1 |
| METHOD OF PREPARING CHARGE OF BALLISTITE SOLID ROCKET FUEL | 2007 |
|
RU2333186C1 |
| METHOD OF PREPARING CHARGE OF BALLISTITE SOLID ROCKET FUEL | 2007 |
|
RU2333189C1 |
| METHOD OF PRODUCING POWDER AND BALLISTITE PROPELLANT | 2005 |
|
RU2288208C1 |
| METHOD OF MANUFACTURE OF THE BALLISTITE SOLID PROPELLANT CHARGE(VERSIONS) | 2005 |
|
RU2300513C2 |
| METHOD OF PREPARING OF BATCH OF SMALL-SIZED CHARGES OF SOLID ROCKET FUEL TO GAS-GENERATOR FOR EJECTION DEVICES OF ROCKET | 2007 |
|
RU2333190C1 |
| METHOD OF PRODUCING LOT OF ROCKET SOLID-PROPELLANT MULTI-GRAIN CHARGES | 2011 |
|
RU2483049C2 |
