FIELD: gas industry.
SUBSTANCE: propellant unit comprises a barrel, a bolt assembly in the bottom part of the barrel with an opening for inlet of working gas from the main line into the inner volume of the barrel, a control destructible shell in the barrel, shutoff and control equipment with a source of working gas and control equipment. Destructible shell is filled with working gas in the propellant volume. Working gas source is made in the form of an electrolytic cell for production of working gas, and a spark discharger is introduced into the composition of the shut-off and control equipment. End part of the barrel is made with the possibility of fixation by the attachment unit of the missile element with the possibility of disconnection from it. Detonation input device is attached to the bottom part of the barrel and is made in the form of a bolt assembly with an inlet hole, which is connected to the inner cavity of the barrel. Axis of symmetry of the inlet hole coincides with the axis of symmetry of the barrel. Element for introduction of detonation into propellant gas volume is made in the form of cylindrical corrector.
EFFECT: increased efficiency of development and performance of experiments, expansion of functional capabilities, as well as increased efficiency during performance of series of experiments.
10 cl, 3 dwg
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Authors
Dates
2025-02-21—Published
2022-12-22—Filed