FIELD: weaponry.
SUBSTANCE: invention relates to rocket engineering. The proposed rocket launcher incorporates a launching tube with a rear end face and water-filled enclosure, the said launching tune being jointed to the carrier and the said enclosure being made from gas-jet-perishable material, for example, polyethylene. The aforesaid water-filled enclosure is fixed directly on the carrier and arranged behind the launching tube rear face downstream of gas jet.
EFFECT: reduced dynamic oscillations of launching tube and rocket in launching.
2 dwg
Title | Year | Author | Number |
---|---|---|---|
ROCKET LAUNCHER | 2005 |
|
RU2295689C1 |
MISSILE LAUNCHING PLANT | 2013 |
|
RU2519606C1 |
DEVICE FOR MISSILE LAUNCHING | 2012 |
|
RU2495353C1 |
MISSILE LAUNCHING PLANT | 2014 |
|
RU2545155C1 |
ROCKET LAUNCHER | 2009 |
|
RU2395053C1 |
ROCKET LAUNCHER | 2015 |
|
RU2577605C1 |
ROCKET LAUNCHER | 2011 |
|
RU2453789C1 |
DEVICE FOR ROCKET LAUNCHING | 2004 |
|
RU2275579C1 |
ROTARY ROCKET LAUNCHER | 2007 |
|
RU2346224C1 |
MISSILE LAUNCHING PLANT | 2014 |
|
RU2545154C1 |
Authors
Dates
2009-01-27—Published
2007-07-26—Filed