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Портал Begell Электронная Бибилиотека e-Книги Журналы Справочники и Сборники статей Коллекции
Journal of Automation and Information Sciences
SJR: 0.238 SNIP: 0.464 CiteScore™: 0.27

ISSN Печать: 1064-2315
ISSN Онлайн: 2163-9337

Выпуски:
Том 51, 2019 Том 50, 2018 Том 49, 2017 Том 48, 2016 Том 47, 2015 Том 46, 2014 Том 45, 2013 Том 44, 2012 Том 43, 2011 Том 42, 2010 Том 41, 2009 Том 40, 2008 Том 39, 2007 Том 38, 2006 Том 37, 2005 Том 36, 2004 Том 35, 2003 Том 34, 2002 Том 33, 2001 Том 32, 2000 Том 31, 1999 Том 30, 1998 Том 29, 1997 Том 28, 1996

Journal of Automation and Information Sciences

DOI: 10.1615/JAutomatInfScien.v40.i1.60
pages 63-70

Specific Features of Performing Space Experiment "Trubka" (The Pipe) in Pressurized Compartment and on External Surface of Russian Segment of the International Space Station

Anatoliy G. Kostornov
I. N. Frantsevich Institute for the Problems of Materials Science, National Academy of Sciences of Ukraine, Kiev, Ukraine
Vyacheslav M. Gulya
Central Research Institute of Engineering, Korolev, Moscow region, Russia
Yuriy A. Elanskiy
State Design Office "Yuzhnoye", Dnepropetrovsk, Ukraine
Anatoliy P. Elchin
RSC Energia, 141070, 4A Lenin Street, Korolev, Moscow Region, Russia
Victor G. Tikhiy
State Design Office "Yuzhnoye", Dnepropetrovsk, Ukraine
Rostislav M. Kopyatkevich
Central Research Institute of Engineering, Korolev, Moscow region, Russia
Gennadiy S. Mishin
Central Research Institute of Engineering, Korolev, Moscow region, Russia
Yuriy M. Prokhorov
Space-Rocket Corporation "Energiya", Korolev, Moscow region, Russia
Gennadiy A. Frolov
Institute for Problems of Material Science of National Academy of Sciences of Ukraine, Kiev, Ukraine
Andrey A. Shapoval
I. N. Frantsevich Institute for the Problems of Materials Science, National Academy of Sciences of Ukraine, Kiev, Ukraine

Краткое описание

We consider state of the works for preparation of scientific equipment for performing space experiment "Trubka" (The Pipe) on external surface and in pressurized compartment of Russian segment of the International Space Station. Thermal state of external surface of transport-cargo space vehicle "Progress-M" is determined. Schemes of flight-experimental plants LEU-TT1 and LEU-TT2 are given. Experimental results confirming working capacity of the block of thermal pipes LEU-TT2 are obtained.


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