FIELD: rocket fuels.
SUBSTANCE: invention provides solid ballistite-type propellant containing nitrocellulose, nitroglycerine, hexogen, chemical resistance stabilizer (centralite or mixture thereof with diphenylamine), industrial or instrumental oil, zinc stearate, sulforicinate E, and adipic acid dinitrile. Propellant is characterized by reduced sensitivity to external effects (shock, friction, shock wave), safety on storage and operation under solid fuel rocket engine conditions, extended application area due to reduced sensitivity to external effects and reduced specific smoke formation power in combustion products at preserved high power characteristics.
EFFECT: improved performance characteristics.
1 tbl
Title | Year | Author | Number |
---|---|---|---|
SOLID ROCKET FUEL | 2001 |
|
RU2207330C2 |
BALLISTITE-TYPE SOLID ROCKET FUEL | 2000 |
|
RU2172730C1 |
SOLID ROCKET FUEL | 1996 |
|
RU2090544C1 |
BALLISTIC ARTILLERY GUN POWDER (VARIANTS) | 2005 |
|
RU2284310C1 |
BALLISTIC PROPELLANT | 2004 |
|
RU2271348C1 |
BALLISTITE PROPELLANT | 2001 |
|
RU2191765C1 |
BALLISTITE PROPELLANT | 2007 |
|
RU2337089C1 |
BALLISTITE FUEL | 2003 |
|
RU2247700C2 |
BALLISTITE FUEL | 2000 |
|
RU2179165C2 |
BALLISTIC-TYPE SOLID PROPELLANT | 2000 |
|
RU2185356C1 |
Authors
Dates
2006-08-10—Published
2004-12-10—Filed