FIELD: rocket fuels.
SUBSTANCE: method comprises applying adhesive sublayer onto fuel block, drying sublayer, placing and centering fuel block in press mold, heating grained thermoplastic armoring material until fluidity state, and injecting the latter into gap between press mold and fuel block. In such case, armoring material is given up to 30% of process refuse of armoring composition disintegrated to characteristic size of armoring material grains. In particular, to starting armoring material having high fluidity factor, refuse material with lower fluidity factor is added and, vice versa, to starting armoring material having low fluidity factor, refuse material with higher fluidity factor is added.
EFFECT: enhanced economical efficiency of process and utilized refuse material.
2 tbl
| Title | Year | Author | Number |
|---|---|---|---|
| METHOD OF ARMORING OF THE SOLID ROCKET PROPELLANT CHARGES BY THE THERMOPLASTIC COMPOUNDS | 2004 |
|
RU2274550C2 |
| METHOD FOR ARMOR PLATING OF SOLID PROPELLANT CHARGES | 2001 |
|
RU2209135C2 |
| METHOD FOR ARMORING OF SOLID-PROPELLANT CHARGE | 2007 |
|
RU2343069C1 |
| METHOD OF ARMORING OF THE SOLID PROPELLANT CHARGES (VERSIONS) | 2006 |
|
RU2317199C1 |
| METHOD OF ARMORING CHARGES OF BALLISTITE-TYPE SOLID ROCKED FUEL | 2004 |
|
RU2259986C1 |
| THERMOPLASTIC LOW-SMOKE ACETYLCELLULOSE-BASED ARMORING COMPOSITION WITH ELEVATED HEAT RESISTANCE | 2005 |
|
RU2276174C1 |
| METHOD OF ARMORING OF CHARGES MADE OUT OF A BALLISTITE SOLID ROCKET PROPELLANT | 2004 |
|
RU2263577C1 |
| METHOD OF MANUFACTURE OF THE GRANULATED ARMORED COMPOSITION BASED ON THE THERMOPLASTIC ELASTOMER USED FOR THE SOLID ROCKET PROPELLANT CHARGES | 2005 |
|
RU2305629C1 |
| METHOD OF ARMORING OF SOLID PROPELLANT CHARGES | 2003 |
|
RU2247655C1 |
| METHOD OF INHIBITING CONICAL CHARGE OF SOLID PROPELLANT ON AUTOMATIC MOULDING MACHINE | 2013 |
|
RU2538841C1 |
