FIELD: engines and pumps.
SUBSTANCE: invention relates to rocket engines and can be used in designing and producing solid-propellant rocket engines. Said engine incorporates housing with omniradial combustion charge arranged therein with gap and igniter fitted on charge front end face side. Charge features circular ledge arranged on charge rear end face edge in contact with housing inner surface. Circular ledge has through cuts made along charge generating line or at angle to it.
EFFECT: higher engine efficiency due to simpler design, better charge ignition and lower smoke formation.
3 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| SOLID-FUEL CHARGE IGNITER FOR ROCKET ENGINE | 2010 |
|
RU2432484C1 |
| SOLID-PROPELLANT ROCKET ENGINE | 2005 |
|
RU2286475C2 |
| SOLID PROPELLANT ROCKET ENGINE (VERSIONS) | 2009 |
|
RU2412369C1 |
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|
RU2282743C2 |
| SOLID-PROPELLANT ROCKET ENGINE | 2010 |
|
RU2438033C1 |
| SOLID-PROPELLANT ROCKET ENGINE | 2005 |
|
RU2305790C1 |
| ROCKET ENGINE SOLID-PROPELLANT CHARGE IGNITER | 2002 |
|
RU2212557C1 |
| SOLID PROPELLANT ROCKET ENGINE | 2008 |
|
RU2383764C1 |
| SOLID-PROPELLANT ROCKET ENGINE | 2003 |
|
RU2247254C1 |
| SOLID-PROPELLANT ROCKET ENGINE | 2001 |
|
RU2213242C2 |
