FIELD: weapons and ammunition.
SUBSTANCE: device for reducing gas-dynamic influence on ground and launching station (LS) contains jet deflector in the form of additional jet propulsion engine (JPE) with elements of fixing, lifting and dropping, nozzle with cylindrical tip. Internal diameter and length of the tip depend upon diameter of critical nozzle, Mach number at nozzle shear, environmental pressure, gas total pressure in additional JPE. The device is connected to LS and by series of sequential pulses of jet stream it performs deflection of jet stream of starting missile from LS.
EFFECT: invention allows increasing safety of missiles launching from LS at the angles close to vertical angle.
2 dwg
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