FIELD: rocketry.
SUBSTANCE: proposed solid-propellant rocket engine has combustion chamber with inserted powder charge and nozzle assembly, bottom and nozzle diaphragms and bottom space with channel to let out gas from bottom space. If nozzle number is even, channel to let out gas from bottom space is made in form of tubes directly connecting bottom space with each second nozzle. If nozzle number is odd, channel to let out gas from bottom space is made in form of tubes directly connecting bottom space with each nozzle, outer diameter of tubes being less than diameter of nozzle critical section, thus forming ring passage cross section.
EFFECT: improved efficiency of holding of inserted powder charge in combustion chamber.
3 dwg
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Authors
Dates
2004-10-27—Published
2002-12-26—Filed