FIELD: weapons and ammunition.
SUBSTANCE: device for launching a guided missile with aerodynamic rudders from the container comprises a lock, a launch control device and pressure accumulators installed in the missile tail, each of which is made in the form of a hull with a pair of nozzles and a pyro cartridge with an igniter squib and controlled slide valve installed in the shell. The launch control device is made in the form of a launch preparation console with the possibility to enter the ambient temperature values, the required speed value, the value of permissible longitudinal missile load, the calculated values of pressure change over time in the accumulators of pressure and overpressure in the launching container shell. The device allows you to control the process of creating optimal pressure within the container and set a certain amount of time between actuations of the pressure accumulators.
EFFECT: reduced weight of the container.
2 cl, 6 dwg
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Authors
Dates
2017-12-22—Published
2016-12-07—Filed