FIELD: weaponry.
SUBSTANCE: invention relates to combat jet equipment and can be used in conducting battle and to fight against terrorists. The proposed jet shell has axially-symmetric casing housing explosive, shell trajectory control system, onboard computer connected to engine controller and fuel tank. Note that the shell incorporates four liquid-fuel gas turbine jet engines. Each of the aforesaid engines comprises, air intake, compressor, combustion chamber and turbine. Note that the compressor rotor and turbine wheel rotor make the engine rotor, while the engine stator is formed by air intake, compressor stator, combustion chamber and supersonic nozzle.
EFFECT: higher shell velocity, range and accuracy along with expanded performances.
4 cl, 7 dwg
Title | Year | Author | Number |
---|---|---|---|
SUPERSONIC BIROTATING JET SHELL | 2007 |
|
RU2338151C1 |
SUPERSONIC MISSILE | 2007 |
|
RU2348894C1 |
SUPERSONIC JET SHELL | 2007 |
|
RU2342628C1 |
SUBSONIC JET SHELL | 2007 |
|
RU2345315C1 |
BIROTATING JET SHELL | 2007 |
|
RU2338150C1 |
CRUISE MISSILE | 2007 |
|
RU2352892C2 |
COMBINED MISSILE | 2007 |
|
RU2348895C2 |
CRUISE MISSILE | 2007 |
|
RU2351888C1 |
AIR BOMB | 2007 |
|
RU2347178C1 |
AVIATION BOMB | 2007 |
|
RU2345318C1 |
Authors
Dates
2009-03-27—Published
2007-04-26—Filed