FIELD: rocket engines.
SUBSTANCE: proposed method of manufacture of solid-propellant charge igniter includes vacuum forming of surface of polymeric film case which is carried out directly on seat in rocket engine housing, for instance in engine cover.
EFFECT: improved mass and dimensional characteristics of rocket engine, simplified technology of manufacture.
7 cl, 3 dwg
Title | Year | Author | Number |
---|---|---|---|
SOLID-PROPELLANT CHARGE IGNITER AND METHOD OF ITS MAKING | 2004 |
|
RU2288371C2 |
ROCKET ENGINE IGNITER | 2001 |
|
RU2185522C1 |
CHARGE IGNITER FOR SOLID-PROPELLANT ROCKET ENGINE | 2005 |
|
RU2309282C2 |
SOLID-PROPELLANT ROCKET ENGINE | 2010 |
|
RU2438033C1 |
ROCKET ENGINE SOLID-PROPELLANT CHARGE IGNITER | 2002 |
|
RU2212557C1 |
METHOD FOR MANUFACTURING OF ANNULAR FILM IGNITER | 2008 |
|
RU2368795C1 |
SOLID-PROPELLANT CHARGE IGNITER | 2011 |
|
RU2476711C1 |
SOLID-FUEL CHARGE IGNITER FOR ROCKET ENGINE | 2010 |
|
RU2432484C1 |
METHOD FOR MAKING CIRCULAR FILM-TYPE IGNITER | 2006 |
|
RU2329392C1 |
SOLID-PROPELLANT CHARGE IGNITER | 1999 |
|
RU2170842C1 |
Authors
Dates
2005-04-27—Published
2003-09-08—Filed