FIELD: weapons and ammunition.
SUBSTANCE: hydrogen bomb comprises axially symmetric body accommodating thermonuclear charge, and control system with blast initiation sensor. Said body accommodates fuel tank, gas turbine engine arranged body axis and comprising air intake, compressor, combustion chamber, turbine, exhaust stage 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. Thermonuclear charge features annular shape and is located concentrically with aforesaid engine. Besides it comprises converter fuse, plutonium or uranium charge, tank with beryllium mix arranged inside gas turbine engine gas exhaust duct and container with deuterium located inside tank with beryllium mix.
EFFECT: higher speed, increased range and accuracy.
6 cl, 4 dwg
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|
RU2480706C2 |
AVIATION BOMB | 2007 |
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AIR BOMB WITH BIROTARY GAS TURBINE ENGINE | 2007 |
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RU2347179C1 |
AVIATION TORPEDO | 2007 |
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RU2345316C1 |
AIRCRAFT TORPEDO | 2007 |
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RU2348003C1 |
AVIATION TORPEDO | 2007 |
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CRUISE MISSILE | 2007 |
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RU2351888C1 |
UNIVERSAL TORPEDO | 2012 |
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RU2477448C1 |
TORPEDO | 2014 |
|
RU2571664C1 |
Authors
Dates
2013-03-10—Published
2011-07-15—Filed