FIELD: engines and pumps.
SUBSTANCE: proposed engine comprises casing with charge. Igniter with pyro composition enclosed in thin-wall tight envelopment is arranged on grid located nearby charge end face. Pyrocartridge with afterburner tube is arranged in casing cover. Afterburner tube edge is spaced apart from igniter envelopment. Igniter envelopment has cylindrical recess made on the side of afterburner tube and aligned with the latter that feature the following relations of recess height h and diameter D of recess from afterburner tube inner diameter d: d≤h≤2d and 3d≤D≤5d.
EFFECT: higher reliability and efficiency.
4 dwg
Title | Year | Author | Number |
---|---|---|---|
CUMULATIVE-HIGH-EXPLOSIVE CHARGE ENGINE | 2018 |
|
RU2675983C1 |
DEVICE TO IGNITE CHARGE OF SOLID-PROPELLANT ROCKET ENGINE | 2012 |
|
RU2500913C1 |
CASE OF SOLID-PROPELLANT ROCKET ENGINE | 2002 |
|
RU2230926C1 |
ROCKET PROJECTILE PULSED MICRO ENGINE | 2008 |
|
RU2382222C1 |
PULSED SOLID-FUEL ENGINE | 2015 |
|
RU2604772C1 |
PYROTECHNIC NITROGEN-GENERATING DEVICE | 2005 |
|
RU2347979C2 |
SOLID-PROPELLANT ROCKET ENGINE START SYSTEM AND PRESSURE INTAKE OF SOLID-PROPELLANT ROCKET ENGINE | 2011 |
|
RU2482321C1 |
GAS GENERATOR SOLID-PROPELLANT CHARGE | 2002 |
|
RU2213245C1 |
SHOOTING DEVICE FOR AIRCRAFT EJECTION SEAT | 2008 |
|
RU2390471C1 |
ROCKET ENGINE IGNITER | 2001 |
|
RU2185522C1 |
Authors
Dates
2012-02-27—Published
2009-12-09—Filed