FIELD: aerospace equipment, solid-fuel jet engines. SUBSTANCE: technical object of invention consists in increased specific thrust pulse of engine, in increased power and simplification of design which are achieved thanks to manufacture of solid-fuel charge in jet engine that includes body, combustion chamber with solid-fuel charge and nozzle in the form of propellant grain. Central combustion chamber is formed in propellant grain in the form of conical recess, additional combustion chambers located in end face part of propellant grain are formed around central chamber. EFFECT: increased specific thrust pulse, increased power and simplification of design of engine. 4 cl, 2 dwg
Title | Year | Author | Number |
---|---|---|---|
REACTIVE PROPELLANT CELLS | 1998 |
|
RU2158837C2 |
SOLID-PROPELLANT JET ENGINE | 1997 |
|
RU2141571C1 |
POWDER ROCKET ENGINE | 2000 |
|
RU2195567C2 |
AIR-JET ENGINE | 2000 |
|
RU2243400C2 |
OPPOSED JET ENGINE | 1998 |
|
RU2151319C1 |
STAROVEROV'S CONICAL ROCKET ENGINE 8 (VERSIONS) AND METHOD OF ITS VERTICAL LAUNCHING (VERSIONS) | 2013 |
|
RU2524793C1 |
ROCKET ENGINE OF SOLID FUEL | 2018 |
|
RU2685751C1 |
METHOD OF STRAIGHT-AND-LEVEL FLAPPING FLIGHT | 1996 |
|
RU2129506C1 |
WING | 1998 |
|
RU2147544C1 |
WINDMILL | 1998 |
|
RU2158848C2 |
Authors
Dates
1999-12-10—Published
1997-09-29—Filed