FIELD: weapons and ammunition.
SUBSTANCE: device comprises a device to form stages of protection and switching of signals arriving into a destruction unit, an electric fuse included into the destruction unit, an input busbar. There is the first, second and third trajectory sensors. Besides, there is a device of energy accumulation, a device of constant time delay, the fourth sensor of time programming. The output of the device to form stages of protection and switching of signals arriving into the destruction unit is connected to the input of the first trajectory sensor, the output of which is connected to the input of the destruction unit electric fuse. The first trajectory sensor is a pressure alarm. The first input of the device to form stages of protection and switching of signals arriving into the destruction unit is connected to the output of the energy accumulation device, the second input - to the output of the second trajectory sensor, the third input - to the output of the third trajectory sensor, and the fourth input - to the output of the fourth sensor of time programming. The second and third trajectory sensors are installed in parallel to each other. The control input of the device to form stages of protection and switching of signals arriving into the destruction unit is connected to the input busbar. The device of constant time delay is installed in the device to form stages of protection and switching of signals arriving into the destruction unit.
EFFECT: invention ensures safety during missile self-destruction both in case of scheduled and non-scheduled launch.
1 dwg
Title | Year | Author | Number |
---|---|---|---|
DEVICE FOR ROCKET SELF-LIQUIDATION | 2007 |
|
RU2343399C1 |
MISSILE SELF-DESTROYING DEVICE | 2006 |
|
RU2316722C1 |
ELECTRONIC FUSE | 2019 |
|
RU2707108C1 |
MULTIMODE FUSE | 2024 |
|
RU2824453C1 |
RADIO FUSE ACCORD-2K FOR SALVO DELAYED ACTION BLASTING OF AMMUNITION WITH OPTICAL-ELECTRON DEVICE ACKNOWLEDGING PRESENCE OF TARGET | 2001 |
|
RU2216709C2 |
MISSILE WITH SPATIAL LIMITATION OF FLIGHT TRAJECTORY AND METHOD OF ITS SELF-DESTRUCTION | 2019 |
|
RU2724152C1 |
MISSILE WITH A SPATIAL RESTRICTION OF THE FLIGHT PATH | 2022 |
|
RU2788218C1 |
DETONATING FUSE OF COMBINED ACTION | 2012 |
|
RU2483274C1 |
METHOD FOR COMBINATION INITIATION OF AMMUNITION AND AMMUNITION WITH COMBINATION INITIATION | 1998 |
|
RU2135947C1 |
DEVICE FOR AUTOMATIC REGULATION OF ELECTRIC TRANSMISSION | 0 |
|
SU1473004A1 |
Authors
Dates
2011-07-10—Published
2010-05-20—Filed