发明名称 УСТРОЙСТВО ДЛЯ ЗАПУСКА РАКЕТ
摘要 FIELD: rocketry, in particular, devices for rocket launching. ^ SUBSTANCE: the device for rocket launching has a flow-through launching tube linked with the carrier, and a flow-through probe fastened on the rear section of the tube. Radial slots that a flow-through in the longitudinal direction are made on the inner surface of the flow-through probe. ^ EFFECT: reduced gas dynamic action on the carrier. ^ 3 dwg
申请公布号 RU2004133546(A) 申请公布日期 2006.04.20
申请号 RU20040133546 申请日期 2004.11.18
申请人 Кириленко Николай Яковлевич (RU) 发明人 Кириленко Николай Яковлевич (RU)
分类号 F41F3/04 主分类号 F41F3/04
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