FIELD: weaponry.
SUBSTANCE: invention relates to ammunition used for bombing the ground, water surface and underwater targets. The proposed air bomb comprises four solid-propellant jet engines and a gas turbine engine. Note that the former are arranged at the bomb rear all along its edges while the latter is fitted along the bomb shell. The said gas turbine runs on fluid propellant and comprises fluid fuel tank, air intake, compressor, combustion chamber and turbine. The bomb is furnished also with the control system, funs drives and built-in computer.
EFFECT: higher speed and range, improved accuracy of bombing and expanded performances.
6 cl 5 dwg
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AVIATION BOMB | 2007 |
|
RU2345318C1 |
AIR BOMB WITH BIROTARY GAS TURBINE ENGINE | 2007 |
|
RU2347179C1 |
AVIATION TORPEDO | 2007 |
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RU2345316C1 |
NUCLEAR BOMB | 2011 |
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RU2480706C2 |
AIRCRAFT TORPEDO | 2007 |
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HYDROGEN BOMB | 2011 |
|
RU2477449C1 |
AVIATION TORPEDO | 2007 |
|
RU2345317C1 |
CRUISE MISSILE | 2007 |
|
RU2351888C1 |
CRUISE MISSILE | 2007 |
|
RU2352892C2 |
COMBINED MISSILE | 2007 |
|
RU2348895C2 |
Authors
Dates
2009-02-20—Published
2007-05-03—Filed