FIELD: transport.
SUBSTANCE: invention relates to aeronautics. In compliance with first version, airship comprises airframe, air chamber 2, self-contained power supply system to produce electric power and heat air chamber air, nuclear liquid-salt reactor 27 with three-circuit heat rejection system made up of circuit 12 for circulation of fuel salt composition melt, circuit 11 for circulation of intermediate salt heat carrier, and circuit of gas heat carrier circulation. In compliance with second version, airship additionally comprises heat exchanger 23, while fuel salt composition melt additionally includes melt of intermediate salt heat carrier. In compliance with third version, airship comprises additionally air chamber 2 enclosed in heat-insulated envelopment. In compliance with third version, airship comprises additionally heat exchanger 23 and air chamber 2 enclosed in heat-insulated envelopment 20.
EFFECT: higher reliability.
12 cl, 6 dwg
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Authors
Dates
2011-01-10—Published
2009-04-03—Filed