FIELD: delivery of gaseous oxygen to spacecraft.
SUBSTANCE: proposed system includes high-pressure bottle and delivery main provided with starting valve, gas reducer, filters-current dischargers and adjusting valve. Filters-current dischargers mounted after starting valve and gas reducer are made in form of screen manufactured from corrosion-resistant metal at low specific resistance. Adjusting valve ensures required rate of oxygen flow through atomizing nozzle fitted at end of delivery main and communicated with consumer.
EFFECT: avoidance of formation of static electricity in oxygen layers; avoidance of fire danger.
1 dwg
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