FIELD: engines and pumps.
SUBSTANCE: double-pulse solid-propellant rocket engine includes front bottom, housing, charges of the second and the first mode, which are installed in it in series, igniters, dividing plate and nozzle. Charge of the second mode represents channel-slot charge the slot cutouts of which are made in pairs so that slot cutouts located opposite each other have various length. Lengths of long and short slot cutouts and their height is determined by ratios protected by this invention.
EFFECT: invention allows providing stable thrust characteristics of rocket engine and improving its reliability.
3 dwg
Title | Year | Author | Number |
---|---|---|---|
SOLID-PROPELLANT ROCKET ENGINE | 2008 |
|
RU2389895C1 |
SOLID PROPELLANT ROCKET ENGINE | 2008 |
|
RU2378525C1 |
SOLID-PROPELLANT ROCKET ENGINE | 2010 |
|
RU2461728C2 |
DUAL-MODE POWER PLANT | 2010 |
|
RU2445492C1 |
SOLID-PROPELLANT ROCKET ENGINE | 2006 |
|
RU2308608C1 |
SOLID PROPELLANT ASCENT ENGINE | 2007 |
|
RU2377431C2 |
SOLID-PROPELLANT ROCKET ENGINE | 2010 |
|
RU2438033C1 |
DUAL-MODE SOLID PROPELLANT ROCKET ENGINE | 2022 |
|
RU2783054C1 |
SOLID-PROPELLANT ROCKET ENGINE | 2007 |
|
RU2336430C1 |
SOLID-PROPELLANT ROCKET ENGINE NOZZLE | 2013 |
|
RU2540190C1 |
Authors
Dates
2011-12-10—Published
2010-05-11—Filed