FIELD: weapons and ammunition.
SUBSTANCE: torpedo comprises axially symmetric body to house explosive device, compressed air bottle, oxidiser and fuel tanks, liquid-propellant rocket engine, control system, onboard computer connected with video camera, controller, transceiver with antenna, and GPS receiver. Said liquid-propellant rocket engine is arranged along body axis and comprises combustion chamber, turbo pump unit with turbine and oxidiser and fuel pumps, oxidiser and fuel tanks communicated via appropriate pipelines with said turbo pump unit. Fast-release tight plug is fitted at the body rear end as well as four steering jet nozzles aligned with liquid-propellant rocket engine and connected with turbine via tubes provided with flow meters and drives.
EFFECT: higher speed, increased range and accuracy.
7 cl, 8 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| ANTIAIRCRAFT MISSILE | 2012 |
|
RU2477445C1 |
| TORPEDO | 2014 |
|
RU2571664C1 |
| ANTIAIRCRAFT MISSILE | 2012 |
|
RU2477446C1 |
| GROUND-TO-AIR MISSILE | 2012 |
|
RU2484418C1 |
| NUCLEAR SUBMARINE AND MARINE-VERSION LIQUID-PROPELLANT ROCKET ENGINE | 2012 |
|
RU2488517C1 |
| NUCLEAR SUBMARINE | 2012 |
|
RU2494004C1 |
| NUCLEAR SUBMARINE AND MARINE-VERSION ROCKET ENGINE | 2011 |
|
RU2466056C1 |
| LIQUID-PROPELLANT ENGINE (VERSIONS) | 2012 |
|
RU2481550C1 |
| LIQUID-PROPELLANT ENGINE | 2011 |
|
RU2466292C1 |
| TURBO-PUMP UNIT OF ROCKET ENGINE | 2012 |
|
RU2481489C1 |
