FIELD: weapons.
SUBSTANCE: present invention pertains to weapons and is meant for use in combat with terrorists. The combined missile has a case with axially symmetrical shape with four stabilisers. Inside the case there is an explosive device, a fuel tank, solid fuel jet engines, fitted in the rear part of the missile on its periphery. Along the axis of the missile there is a gas-turbine engine, working on liquid fuel and with an air intake, compressor, combustion chamber and a turbine. The fuel tank is anchor ring shaped and is joined by a fuel line, fitted with a fuel pump, to the combustion chamber.
EFFECT: increase in missile velocity, range and target accuracy and widening of functional capabilities of the missile.
6 cl, 4 dwg
Title | Year | Author | Number |
---|---|---|---|
SUPERSONIC JET SHELL | 2007 |
|
RU2342628C1 |
CRUISE MISSILE | 2007 |
|
RU2351888C1 |
CRUISE MISSILE | 2007 |
|
RU2352892C2 |
AIR BOMB | 2007 |
|
RU2347178C1 |
SUBSONIC JET SHELL | 2007 |
|
RU2345315C1 |
SUPERSONIC BIROTATING JET SHELL | 2007 |
|
RU2338151C1 |
AVIATION BOMB | 2007 |
|
RU2345318C1 |
SUPERSONIC MISSILE | 2007 |
|
RU2348894C1 |
SUPERSONIC JET SHELL | 2007 |
|
RU2350893C2 |
BIROTATING JET SHELL | 2007 |
|
RU2338150C1 |
Authors
Dates
2009-03-10—Published
2007-05-03—Filed