FIELD: ground equipment for control of environment parameters of space rocket articles.
SUBSTANCE: proposed method includes delivery of gas component to upper part of head module and discharge of it from lower part. Excessive pressure is built up in head module. Device proposed for realization of this method includes flow activator used for delivery of gas component to head module, filter for cleaning the gas components delivered to flow activator inlet, gas ducts and thermostatting members for maintenance of head conditions in head module. Gas component flow divider included in head module is connected with thermostatting members by means of gas ducts. Gas flow divider is secured in upper part of nose fairing of head module. Gas component discharge hatch is provided in lower part of nose fairing.
EFFECT: high cleanness of head module; enhanced maintenance of heat conditions of space rocket before withdrawal of service tower.
3 cl, 1 dwg
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