FIELD: procedure of manufacture of solid-propellant charges, applicable for application of armor coating on the side surface of the charges.
SUBSTANCE: the mould has a die, cover and a pusher, it is provided with two half-bushes with a tapered outer surface, conjugate to the tapered inner surface of the die and with compression springs and guide bushes installed in the cavity of joint of the half-bushes.
EFFECT: enhanced reliability of estimation of the condition of the building foundations.
6 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| CASTING MOLD | 2003 |
|
RU2256555C1 |
| CASTING MOLD | 2001 |
|
RU2209728C2 |
| SOLID FUEL CHARGE ARMORING APPARATUS | 2001 |
|
RU2208005C2 |
| METHOD FOR ARMOR PLATING OF SOLID PROPELLANT CHARGES | 2001 |
|
RU2209135C2 |
| METHOD OF SOLID ROCKET PROPELLANT CHARGES ARMORING | 2001 |
|
RU2219148C2 |
| METHOD FOR ARMORING OF SOLID-PROPELLANT CHARGE | 2007 |
|
RU2343069C1 |
| INSERTED SLOW-BURNING SOLID PROPELLANT CHARGE | 2002 |
|
RU2215722C2 |
| METHOD OF ARMORING OF THE SOLID PROPELLANT CHARGES (VERSIONS) | 2006 |
|
RU2317199C1 |
| METHOD FOR ARMORING A HARD ROCKET FUEL CHARGE | 2004 |
|
RU2259919C1 |
| PROTECTIVE-ADHESION SUBLAYER TO ARMOR THE CHARGES OF SOLID ROCKET PROPELLANT | 2001 |
|
RU2217460C2 |
Authors
Dates
2005-03-20—Published
2003-10-08—Filed