| 摘要 |
FIELD: rocketry, in particular, take-off of missiles from air missile carriers. ^ SUBSTANCE: the winged missile is suspended from an aircraft missile launcher I a position turned by 45 deg. about the longitudinal axis, after the take-off the missile is turned to the initial flight position. The missile air-intake fairing is released by sending a pulse to it in the direction of winged missile motion up to execution of the mentioned banked turn. In the initial flight section the control of the winged missile motion is accomplished with the aid of joint operation of the missile aerodynamic control surfaces and the fin controls. ^ EFFECT: reduced terms and costs of perfection of production of the winged missile aircraft version, provided compact arrangement of the winged missiles on aircraft launchers without folding of the "plus-shaped" wing and fin assembly, as well as provided a reliable and safe take-off from the aircraft. ^ 6 dwg |
