FIELD: engines.
SUBSTANCE: invention relates to rocket propulsion systems on solid fuel. Method of accelerating flying device, including a self-moving solid-fuel element (frameless rocket engine) with a flight stabilizer, wherein at start of flying device complete combustion of frameless rocket engine is provided, at that, a hollow cylindrical cartridge with a blind front cover is used as an engine, made of solid fuel with combustion rate of not less than 30 mm/s, herewith, at start-up of the device on one stabilizer several frameless rocket engines are placed in parallel to each other and their synchronous combustion in an acceleration section of the flight is provided.
EFFECT: invention provides increase in maximum speed and flight range of the self-propelled solid-fuel elements, used for active influence on atmospheric processes.
1 cl, 1 tbl, 6 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| STAROVERV'S-8 ROCKET ENGINE (VERSIONS) | 2012 |
|
RU2561820C2 |
| METHOD FOR LAUNCHING GUIDED PROJECTILE AND GUIDED PROJECTILE FOR ITS IMPLEMENTATION | 2007 |
|
RU2358231C2 |
| SOLID-PROPELLANT ROCKET ENGINE FOR GUIDED PROJECTILE AND SOLID PROPELLANT IGNITOR | 1994 |
|
RU2079689C1 |
| GUIDED MISSILE SOLID-PROPELLANT ROCKET ENGINE, SOLID PROPELLANT IGNITER AND ROCKET ENGINE NOZZLE ASSEMBLY | 2008 |
|
RU2351788C1 |
| STAROVEROV'S CONICAL ROCKET ENGINE 8 (VERSIONS) AND METHOD OF ITS VERTICAL LAUNCHING (VERSIONS) | 2013 |
|
RU2524793C1 |
| BIRD REPELLING METHOD | 2002 |
|
RU2250611C2 |
| BULLET WITH REACTIVE LAUNCHED CARTRIDGE | 2020 |
|
RU2777720C2 |
| METHOD FOR ACTUATING UPON PROCESSES OF SELF-CLEANING OF ATMOSPHERE FROM AEROSOL INGREDIENTS | 2001 |
|
RU2202172C2 |
| HYDROMETEOROLOGICAL ROCKET PROJECTILE | 1995 |
|
RU2090832C1 |
| BIRD REPELLING METHOD | 1998 |
|
RU2140151C1 |
