DEVICE FOR ROCKET FASTENING AGAINST LONGITUDINAL DISPLACEMENTS

摘要

FIELD: mechanical engineering. SUBSTANCE: device for rocket fastening on launcher uses a leverage with a blade installed opposite the engine nozzle. The device is furnished with a roll having a T-shaped cut-out, which is linked to the lever and fastened to the blade. The link end that is engageable with the roll is T-shaped. EFFECT: enhanced reliability of rocket fastening and its release at engine starting. 2 dwg