FIELD: rocketry and space engineering; devices for relief of components from cryogenic stages.
SUBSTANCE: proposed device has two symmetrical tubes connected by means of adapter. Mounted at outlets of these tubes are screen nozzles. Proposed device makes it possible to reduce difference in thrust at tube outlets, thus reducing disturbance acting on cryogenic stage at relief of gaseous component from it.
EFFECT: enhanced efficiency.
2 dwg
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Authors
Dates
2006-11-10—Published
2004-08-23—Filed