FIELD: rocketry, applicable for combustion of a solid propellant charge.
SUBSTANCE: the method consists in vertical installation of the solid rocket engine, fastening of it to a footpad and combustion of the charge. The rocket engine is installed directly in the shaft of the launching silo, where combustion of the charge is performed. The rocket engine is installed with the nozzle up, and the nozzle is closed with a sealed end-cap. Then, the rocket engine is connected to the stationary launch control panel and to the engine maintenance recording system, the shaft of the launching silo is filled with an inert liquid up to the upper lever, and ignition of the charge is initiated.
EFFECT: reduced expenditures on preparation and combustion of solid propellant charges.
1 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| METHOD OF ROCKET ENGINE SOLID FUEL UTILISATION | 2007 |
|
RU2345283C1 |
| METHOD OF AFTERBURNING OF INCOMPLETELY COMBUSTED PRODUCTS AT RECYCLING OF SOLID-PROPELLANT ROCKET ENGINES | 2004 |
|
RU2278987C1 |
| AFTERBURNING METHOD OF INCOMPLETE COMBUSTION PRODUCTS AT UTILISATION OF SOLID-PROPELLANT ROCKET ENGINE | 2010 |
|
RU2428578C1 |
| ROCKET ENGINE OF ROCKET-ASSISTED PROJECTILE | 2016 |
|
RU2620613C1 |
| METHOD OF INCREASING THE DISTANCE OF THE ROCKET-PROPELLED GRENADE | 2017 |
|
RU2647256C1 |
| METHOD OF DESTRUCTION OF SOLID PROPELLANT CHARGES | 1997 |
|
RU2123991C1 |
| PROCEDURE TO LIQUIDATE SOLID FUEL CHARGE | 2000 |
|
RU2169282C1 |
| METHOD OF EXPERIMENTAL ESTIMATION OF LAUNCHING AIRCRAFT MISSILE WITH SOLID PROPELLANT CHARGE | 2011 |
|
RU2472963C1 |
| SOLID PROPELLANT ROCKET ENGINE | 2008 |
|
RU2383764C1 |
| PLANT FOR RECOVERY OF ROCKET SOLID PROPELLANT CHARGES | 1995 |
|
RU2087804C1 |
