FIELD: weaponry.
SUBSTANCE: invention relates combat equipment and is intended for bombardment of the ground, water surface and underwater targets. The aviation bomb represents an axisymmetric body with four fins housing an explosion device, a control system, a fuel tank, a fluid-propellant gas-turbine engine comprising an air intake, a compressor, a combustion chamber and a turbine. Note that the fuel tank communicates, via a fuel line accommodating a fuel pump with a drive, with the aforesaid combustion chamber. The gas turbine outlet accommodates a central nozzle. Note also that four side nozzles are connected to the aforesaid gas turbine outlet via adjusting devices. Mind that the control system incorporates the fins drives and onboard computer.
EFFECT: increased speed, range and accuracy of bombing, expanded potentialities of bombs.
7 cl, 6 dwg
Title | Year | Author | Number |
---|---|---|---|
AIR BOMB WITH BIROTARY GAS TURBINE ENGINE | 2007 |
|
RU2347179C1 |
AIR BOMB | 2007 |
|
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AVIATION TORPEDO | 2007 |
|
RU2345316C1 |
NUCLEAR BOMB | 2011 |
|
RU2480706C2 |
AIRCRAFT TORPEDO | 2007 |
|
RU2348003C1 |
HYDROGEN BOMB | 2011 |
|
RU2477449C1 |
AVIATION TORPEDO | 2007 |
|
RU2345317C1 |
CRUISE MISSILE | 2007 |
|
RU2351888C1 |
TORPEDO | 2014 |
|
RU2571664C1 |
UNIVERSAL TORPEDO | 2012 |
|
RU2477448C1 |
Authors
Dates
2009-01-27—Published
2007-05-03—Filed