FIELD: test equipment.
SUBSTANCE: invention relates to launchers, namely to test beds. The stabilising device of the monorail rocket carriage (RC) of the rocket track contains a wing in the form of the pointed plate, shaft, device or determination of tilt with a gyroscope and two contact sensors, wing rotation device in the form of the stepper motor or two pyro-pushers with cylinders, rods and powder charges, wing rotation device control unit with the power supply, shoe, chock, burning system for the powder charge of pyro-pushers as an ignition powder charge, pair of rocket motors (RM). A wing is established in a vertical plane and during RC motion the incidence angle variation is eliminated, a pair of RMs is installed and during RC motion the tilt is eliminated.
EFFECT: invention allows to stabilise a tilt along the whole length of the accelerating section.
15 cl, 25 dwg
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