FIELD: military equipment; rockets with separable cluster nose cones; designing units for correction of time of opening and separation of rocket nose cones. SUBSTANCE: proposed device has accelerometer and computer of error for time of opening or separation of nose cone; accelerometer is provided with two sensitive elements with oppositely oriented sensitivity axes and difference signal separation unit. At output of this unit, initial difference signal memory unit is provided; correction computer input is connected with unit for subtraction of accelerometer signal; output of memory unit is connected to input of signal subtraction unit; outputs of sensitive elements are simultaneously connected to input of difference signal separation unit and signal subtraction unit. EFFECT: improved of rocket firing efficiency by 20 to 30% due to enhanced accuracy of determination of moment of separation or opening of rocket nose cone. 1 dwg
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Authors
Dates
2002-03-27—Published
2001-04-12—Filed