FIELD: rocket propellants. SUBSTANCE: proposed solid-propellant charge is made in form of bundle of tubes or other shape members connected with engine chamber bottom by means of noncombustible polymeric material. One or several slots of variable section decreasing in direction of charge are made on surface of bottom. Summary area of slots is 0.4-0.7 of bottom area. EFFECT: improved reliability of charges in operation, simplified design, reduced labor input in manufacture and assembling with engine. 2 dwg
Title | Year | Author | Number |
---|---|---|---|
CHARGE OF A SOLID ROCKET FUEL | 2006 |
|
RU2316669C2 |
ROCKET ENGINE OF IMPULSE VERNIER UNIT | 2005 |
|
RU2289034C1 |
METHOD FOR MANUFACTURE OF SOLID-PROPELLANT CHARGES | 1999 |
|
RU2183606C2 |
SOLID ROCKET FUEL CHARGE MANUFACTURE METHOD | 2003 |
|
RU2259980C1 |
FAST-HARDENING STRENGTHENING COMPOSITION FOR FIXING FUEL CELLS WITH BOTTOM OF ROCKET ENGINE | 1999 |
|
RU2167903C2 |
BRUSH-TYPE CHARGE MADE OUT OF THE BALLISTITE SOLID ROCKET PROPELLANT WITH THE IGNITER | 2005 |
|
RU2312094C2 |
SOLID-PROPELLANT CHARGE | 2010 |
|
RU2449156C2 |
COMPOSITION OF BINDING SUBSTANCE FOR MANUFACTURE OF THE BRUSH TYPE PRODUCTS | 2004 |
|
RU2264427C1 |
POWDER CHARGE OF SOLID ROCKET FUEL | 2007 |
|
RU2357095C1 |
ROCKET SOLID PROPELLANT CHARGE | 2002 |
|
RU2216641C1 |
Authors
Dates
2003-08-27—Published
2002-02-19—Filed