FIELD: weapons and ammunition.
SUBSTANCE: launcher rocket comprises rocket engine with annular or cylindrical channel or annular inhibited grains, fire section, two or more jet nozzles, two tandem shaped charges and contactless laser fuse. Engine incorporates aligned and misaligned layers of propellant and crosswise flat or concave layers of propellant. Propellant layers different in depth, combustion rate and heat release. Rocket launcher comprises tubular guide, revolver drum and mechanism, lever and rod with blade, and spring. Rod with blade includes roller to engage with zigzag-like groove. Spring-loaded ratchets are fitted on groove branches.
EFFECT: higher accuracy of fire.
17 cl, 11 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| STAROVEROV'S CONICAL ROCKET ENGINE 8 (VERSIONS) AND METHOD OF ITS VERTICAL LAUNCHING (VERSIONS) | 2013 |
|
RU2524793C1 |
| STAROVERV'S-8 ROCKET ENGINE (VERSIONS) | 2012 |
|
RU2561820C2 |
| BODYLESS ENGINE (VERSIONS) AND METHOD OF ITS FABRICATION | 2009 |
|
RU2398125C1 |
| UNCASED MOTOR WITH SELF-FEEDING | 2010 |
|
RU2431052C1 |
| STAROVEROV'S ROCKET ENGINE-13a | 2014 |
|
RU2570991C1 |
| STAROVEROV'S ROCKET ENGINE-6 (VERSIONS) | 2012 |
|
RU2570913C2 |
| ROCKET WITH FRAMELESS MOTOR /VERSIONS/ | 2011 |
|
RU2482436C1 |
| MISSILE WITH CASELESS NOZZLELESS ENG-IGNITION ENGINE (VERSIONS) | 2012 |
|
RU2494340C1 |
| DISPLACEMENT-TYPE LIQUID-PROPELLANT ROCKET (VERSIONS) | 2011 |
|
RU2468333C1 |
| STAROVEROV'S PROPELLANT-6 | 2014 |
|
RU2570010C2 |
