FIELD: weapons and ammunition.
SUBSTANCE: cruise missile comprises axisymmetric casing with four wings-stabilisers that accommodates explosive, liquid-propellant engine furnished with air intake, compressor, turbine fuel tank communicating, via a pipeline, with the combustion chamber, and the control system. Proposed cruise missile comprises also four solid-propellant jet engines arranged at the casing rear along its edges. The liquid-propellant engine represents a gas turbine engine located along the casing axis. The fuel tank is arranged inside the casing. Note that the fuel pipeline accommodates fuel pump with its drive. Note also that the control system comprises the stabilisers drives and onboard computer.
EFFECT: increased speed, range and accuracy of hitting.
6 cl, 3 dwg
Title | Year | Author | Number |
---|---|---|---|
CRUISE MISSILE | 2007 |
|
RU2352892C2 |
SUPERSONIC JET SHELL | 2007 |
|
RU2342628C1 |
COMBINED MISSILE | 2007 |
|
RU2348895C2 |
AIR BOMB | 2007 |
|
RU2347178C1 |
SUPERSONIC BIROTATING JET SHELL | 2007 |
|
RU2338151C1 |
SUBSONIC JET SHELL | 2007 |
|
RU2345315C1 |
SUPERSONIC MISSILE | 2007 |
|
RU2348894C1 |
SUPERSONIC JET SHELL | 2007 |
|
RU2350893C2 |
AVIATION BOMB | 2007 |
|
RU2345318C1 |
AVIATION TORPEDO | 2007 |
|
RU2345316C1 |
Authors
Dates
2009-04-10—Published
2007-06-01—Filed