| 摘要 |
FIELD: rocketry, in particular, devices for rocket launching. ^ SUBSTANCE: the device for rocket launching has a flow-through launching tube having the front and rear end faces and linked with the carrier. The rear end face of the launching tube is made in the form of an oblique cut, whose plane is perpendicular to the vertical plane. The oblique cut together with the launching tube forms an oblique-cut probe, whose largest generator is positioned underneath. ^ EFFECT: reduced gas dynamic action on the carrier. ^ 2 dwg |
