FIELD: tracking of space objects. SUBSTANCE: gear has source of air supply in the form of compressed air receivers, supply pipe- line laid along umbilical tower of starter and joined to aboard releasable connector located on side surface of space object. Electric air heater and cooler are put on supply pipe-line. Tank with liquid nitrogen, gas generator and nitrogen electric heater are connected in sequence via gate to supply pipe-line after electric air heater. Tank with nitrogen is connected via gate to supply pipe-line between controlled valves and pressure regulator. Aboard releasable connector located on side surface of space object is connected to supply pipe-line laid along umbilical tower of starter. EFFECT: enhanced efficiency, reliability and fire safety of rocket carrier fueled with liquid hydrogen. 1 dwg
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