FIELD: rocketry. SUBSTANCE: rocket engine nozzle cover includes pressure adjusting valve which is kinematically linked with piston by ball lock; piston is located in cylinder; one member of piston pair is gas-permeable. EFFECT: satisfying all requirements of standard situation and emergency situation of engine flooding; enhanced reliability; low cost; simplified construction. 1 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| DEVICE FOR SEALING OF JET ENGINE NOZZLE | 2001 |
|
RU2195628C1 |
| ROCKET ENGINE NOZZLE PACKING | 2010 |
|
RU2430257C1 |
| ROCKET ENGINE NOZZLE SEALING DEVISE | 2001 |
|
RU2213241C2 |
| SOLID-PROPELLANT ROCKET ENGINE PLUG | 2010 |
|
RU2443897C1 |
| PROPULSION INSTALLATION | 2010 |
|
RU2428580C1 |
| SOLID-FUEL ROCKET ENGINE | 1997 |
|
RU2134814C1 |
| SOLID-PROPELLANT ROCKET ENGINE | 1998 |
|
RU2153093C1 |
| SOLID-PROPELLANT ROCKET ENGINE | 2000 |
|
RU2170838C1 |
| ROCKET ENGINE EXPANDABLE NOZZLE | 2001 |
|
RU2213239C2 |
| METHOD OF MISSILE LAUNCHING FROM SUBMARINE, SURFACE CRAFT AND GROUND CARRIERS FROM LAUNCHING FACILITY ON WATER AND LAUNCHING FACILITY FOR THIS METHOD IMPLEMENTATION | 2012 |
|
RU2536961C2 |
