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
| Title | Year | Author | Number |
|---|---|---|---|
| INSTALLATION TO LAUNCH ROCKETS FROM MOON AND METHOD OF PREPARING ROCKET FOR LAUNCHING | 2007 |
|
RU2354593C1 |
| SEA PLATFORM FOR LAUNCHING ROCKETS AND METHOD OF PREPARATION OF ROCKET FOR LAUNCHING | 2007 |
|
RU2345925C1 |
| AIRCRAFT WING | 2014 |
|
RU2554026C1 |
| LAUNCHING DEVICE FOR ROCKET WITH MULTISTAGE ENGINES | 2010 |
|
RU2423300C1 |
| SEA PLATFORM TO LAUNCH ROCKETS | 2007 |
|
RU2338659C1 |
| METHOD FOR REDUCING GAS-DYNAMIC INFLUENCE ON GROUND OF START POSITION AND LAUNCHING STATION OF STARTING MISSILE JET STREAM AT ANGLES CLOSE TO VERTICAL ANGLE AND DEVICE FOR ITS IMPLEMENTATION | 2012 |
|
RU2481540C1 |
| LAUNCH FACILITY FOR LAUNCH OF CARRIER ROCKET WITH SOLID FUEL ACCELERATORS | 2022 |
|
RU2796178C1 |
| VERTICAL START TRANSPORTATION SYSTEM | 1994 |
|
RU2094330C1 |
| AIRCRAFT WING | 2013 |
|
RU2539440C1 |
| METHOD FOR REDUCING THE DESTRUCTIVE EFFECT ON ELEMENTS OF THE LAUNCH PAD AND THE LAUNCH STRUCTURE DURING THE LAUNCH OF A LAUNCH VEHICLE | 2021 |
|
RU2773482C1 |
