FIELD: transport.
SUBSTANCE: proposed invention relates to aerospace engineering, namely to rocket unit engine plant. Proposed power plant comprises oxidiser and fuel tanks to feed fuel to sustainer engine, pressure signalisers communicated via pipelines with oxidiser tank to maintain oxidiser tank by control system. Said oxidiser tank pressure signalisers are arranged in tight case chambers and furnished with pressure seals and sealed connectors welded into said cases. Pressure inside said sealed cases equals the Earth atmospheric pressure. In space, pressure signaliser signals are sent into control systems when oxidiser tank pressure equals or exceeds that of the cases.
EFFECT: faultless start on engines.
2 dwg
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