FIELD: weapons and ammunition.
SUBSTANCE: nuclear bomb comprises axially symmetric body with tail fins accommodating thermonuclear charge, and control system with blast initiation sensor. Vessel with fuel is arranged inside said body. Gas turbine engine running on liquid fuel is mounted along body axis to comprise air intake, compressor, combustion chamber, turbine, gas duct and nozzle. Fuel tank is connected with combustion chamber via fuel line with driven fuel pump. Control system comprises onboard computer, tail fins drives, and blast initiation sensors. Nuclear charge features annular shape and is arranged concentrically with gas turbine engine.
EFFECT: higher speed, increased range and accuracy.
7 cl, 4 dwg
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RU2477449C1 |
AVIATION BOMB | 2007 |
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AIRCRAFT TORPEDO | 2007 |
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AIR BOMB | 2007 |
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RU2347178C1 |
AIR BOMB WITH BIROTARY GAS TURBINE ENGINE | 2007 |
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RU2347179C1 |
AVIATION TORPEDO | 2007 |
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CRUISE MISSILE | 2007 |
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UNIVERSAL TORPEDO | 2012 |
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TORPEDO | 2014 |
|
RU2571664C1 |
Authors
Dates
2013-04-27—Published
2011-07-15—Filed