FIELD: military equipment, in particular, missiles with separating (cassette) nose cones. SUBSTANCE: device uses an accelerometer, computer and a time-delay mechanism set to the nominal time of opening (separation), it is furnished with a delay element, threshold element and a switch; the inputs of the delay element and threshold element are connected to the computer output, the threshold element output is connected to the control input of the switch, via whose break contacts the input of the time-delay mechanism is connected to the delay element output; the time delay in the delay element exceeds the summary operating time of the threshold element and switch. EFFECT: enhanced efficiency of fire of salvo systems due to enhanced reliability of timely separation or opening of missile nose cone over the target area. 1 dwg
Title | Year | Author | Number |
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ROCKET | 1998 |
|
RU2125704C1 |
DEVICE FOR FORMING TIME OF CORRECTION OF OPENING OR SEPARATION OF ROCKET NOSE CONE | 2001 |
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METHOD OF SETTING TIME OF CORRECTING ROCKET WARHEAD OPENING OR SEPARATION | 2008 |
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DEVICE TO FORM TIME OF CORRECTING MISSILE HEAD SEPARATION | 2007 |
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ROCKET | 1998 |
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GYROSCOPIC HORIZON FOR AUTOMATED FIRE CONTROL SYSTEM | 2000 |
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ROCKET | 1998 |
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PACK HEAD | 1998 |
|
RU2138007C1 |
Authors
Dates
1999-02-10—Published
1998-03-16—Filed