| 摘要 |
FIELD: rocketry. ^ SUBSTANCE: the device has a flow-through launching tube with a probe installed in the rear section of the launching tube, coupled to the carrier. The probe is coupled to the launching tube by means of drive mechanisms, whose shafts are located in the planes passing through the probe axis, and the probe and the launching tube are made with formation of a spherical hinge. ^ EFFECT: provided adjustment of the value of the compensating gas-dynamic force on the launching tube at a missile take-off. ^ 2 dwg |
