naa a22 4500 510761860 CHVBK 20180411083142.0 cr unu---uuuuu 180411e20131201xx s 000 0 eng 10.1134/S0040601513140024 doi (NATIONALLICENCE)springer-10.1134/S0040601513140024 Gribkov A. Korolev Rocket and Space Corporation Energiya, ul. Lenina 4a, 141070, Korolev, Moscow oblast, Russia aut Large-size heat pipes intended for use in a megawatt-class space nuclear power system [Elektronische Daten] [A. Gribkov] The schematic design of a space nuclear power system is suggested that is fitted with a radiating cooler, which deploys and forms a part of the radiation protection cone once a spacecraft has been inserted into its orbit. The principle of selecting a design of a capillary structure for heat pipes with high thermal output (hundreds of kilowatts) is proposed. Comparison is drawn between heat pipes having the proposed and the conventional design. The advantages of the proposed design of heat pipes are shown by calculation results. Pleiades Publishing, Inc., 2013 Thermal Engineering Springer US; http://www.springer-ny.com 60/14(2013-12-01), 1061-1065 0040-6015 60:14<1061 2013 60 11509 https://doi.org/10.1134/S0040601513140024 text/html Onlinezugriff via DOI 1 research-article jats NATIONALLICENCE 856 40 https://doi.org/10.1134/S0040601513140024 text/html Onlinezugriff via DOI NATIONALLICENCE 100 1- Gribkov A. Korolev Rocket and Space Corporation Energiya, ul. Lenina 4a, 141070, Korolev, Moscow oblast, Russia aut NATIONALLICENCE 773 0- Thermal Engineering Springer US; http://www.springer-ny.com 60/14(2013-12-01), 1061-1065 0040-6015 60:14<1061 2013 60 11509 Metadata rights reserved Springer special CC-BY-NC licence nationallicence BK010053 XK010053 XK010000 NATIONALLICENCE NATIONALLICENCE NL-springer