FIELD: manufacture of inhibited solid propellant charges. SUBSTANCE: proposed slow-burning solid propellant charge on base of ammonium nitrate and acetyl cellulose binder is inhibited by two-layer coat on side surface and coat on end surface; two-layer coat applied to side surface includes layer of thermoplastic inhibiting compound with asbo-lavsan fabric coat over it; coat applied to end surface is made from thermoplastic inhibiting compound. Thermoplastic inhibiting compound is made from the same composition as acetyl cellulose binder of propellant. EFFECT: enhanced fire and erosion resistance. 2 cl, 1 dwg
Title | Year | Author | Number |
---|---|---|---|
METHOD OF INHIBITING THERMOPLASTIC PROPELLANT CHARGE | 2002 |
|
RU2215723C2 |
ARMORING COMPOUND FOR BALLISTATE SOLID FUEL INSERT CHARGE THERMOPLASTIC COATING | 2002 |
|
RU2217458C1 |
ARMORING COMPOSITION | 2001 |
|
RU2179989C1 |
THERMOPLASTIC LOW-SMOKE ACETYLCELLULOSE-BASED ARMORING COMPOSITION WITH ELEVATED HEAT RESISTANCE | 2005 |
|
RU2276174C1 |
METHOD OF PRODUCING AUXILIARY ARMORED CHARGE OF BALLISTIC ROCKET FUEL | 2007 |
|
RU2345977C1 |
METHOD OF ARMORING OF CHARGES MADE OUT OF A BALLISTITE SOLID ROCKET PROPELLANT | 2004 |
|
RU2263577C1 |
METHOD OF MANUFACTURING REMOVABLE ARMORED SOLID MIXED PROPELLANT CHARGE | 2006 |
|
RU2315741C1 |
INHIBITING COMPOSITION FOR SOLID ROCKET FUEL CHARGES | 2001 |
|
RU2208007C2 |
PROTECTIVE-ADHESION SUBLAYER TO ARMOR THE CHARGES OF SOLID ROCKET PROPELLANT | 2001 |
|
RU2217460C2 |
SOLID-PROPELLANT CHARGE FOR ROCKET ENGINE | 1999 |
|
RU2164616C1 |
Authors
Dates
2003-11-10—Published
2002-01-11—Filed