FIELD: weapons.
SUBSTANCE: invention relates to rocketry and serves to launch rockets. Proposed launcher comprises flow launching tube 1 coupled with carrier 2 and diffuser 4 fixed at outlet of tube 1. Diffuser inner surface has at least one circular recess arranged in the plane perpendicular to launching tube axis.
EFFECT: stable structure of gas flow expansion that provides for reduced gas dynamic pressure on carrier in rocket starting.
2 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| ROCKET LAUNCHER | 2011 |
|
RU2453789C1 |
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|
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| MISSILE LAUNCHER | 2006 |
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| DEVICE FOR ROCKET LAUNCHING | 2004 |
|
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| DEVICE FOR LAUNCHING MISSILES | 2011 |
|
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| ROCKET LAUNCHER | 2005 |
|
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| ROCKET LAUNCHER | 2008 |
|
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| ROCKET LAUNCHER | 2015 |
|
RU2577586C1 |
| ROTARY ROCKET LAUNCHER | 2007 |
|
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| MISSILE LAUNCHING PLANT | 2014 |
|
RU2545155C1 |
