FIELD: cosmonautics.
SUBSTANCE: invention is related to the field of scale rocket modeling. Launcher comprises detachable ejector nozzle, installed between nozzle for rocket gases outflow and hole in start plate for drain of gases into gas-outlet channel. Ejector nozzle also comprises support element for installation of rocket and may be equipped with funnel for connection of gas jets from several rocket nozzles into one common jet. Ejector nozzle may also be installed with the possibility of detachment from start plate, is connected by means of flexible cord with counterweight having springy section, besides cord rounds block fixed in upper part of auxiliary mast. Support element may be equipped with accessory for coupling with rocket.
EFFECT: increased traction at the moment of rocket launching.
4 cl, 8 dwg
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