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141. Kinematics of galaxies: supplement
We present a catalogue of galaxies for which spatially resolved data on their internal kinematics have been published; there is no apriori restriction regarding their morphological type. The catalogue lists the references to the articles where the data are published, as well as a coded description of these data: observed emission (E) or absorption (A) data, optical (O) or radio (R) data, velocity (V) or velocity dispersion (D), radial profile (1) or 2D field (2). ...
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Ссылки http://neptun.sai.msu.su/~zasov/comcat.htm -- 2.4 Кб -- 15.01.1999
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142. Космическая филателия
... We guess it's almost impossible to create the site nowadays where all space relative philatelic materials (postage stamps, stationary, postal marks etc.) would be registered and presented. ... We tried to make such a step in April 2005, placing at the site first images of postage stamps with portraits of astronauts (cosmonauts, spacionauts, taikonauts:). ... All illustrative material (or simply speaking, all scans of stamps) are grouped in four sections: Countries , Years , Astronauts and Flights . ...
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Ссылки http://www.astronaut.ru/philo/main-e.htm -- 8.6 Кб -- 15.04.2012
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143. Обеспечение управляемого спуска с орбиты орбитального пилотируемого комплекса
... Space research, space communication including TV and radio communication with using satellite systems, Earth and ecological monitoring, the use of satellite, navigation and topogeodesic systems, manned missions, material production in space and lots of other operations could be related to space activity. ... A special 5-year program was developed involving regular Shuttle missions with join crews. ... БИК 2-3 system and "Symbol D" system telemetry data are used to control the Station; . ...
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Ссылки http://www.mcc.rsa.ru/www_old/Mir/www_eng/doklad/doklad_koptev.htm -- 41.0 Кб -- 28.05.2014
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144. http://www.kiam1.rssi.ru/pubs/AAS_09-103.pdf
... 23 Algorithm fo r evalua tion of two burn maneuv ers using linearity Input information: ( t t E1 , rEI , v t1L , t E2 2L ( ) EI )T )T the time and the state vector of initial orbit for this time ; interval of possible thrusts for transition from initial orbit to the transfer on e; the time and the state vector of the target orbit for this time ; ... We cal culate the state vector for the initial orbit for the time t1a and the target one for the time t2 a . ...
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Ссылки http://www.kiam1.rssi.ru/pubs/AAS_09-103.pdf -- 2056.5 Кб -- 05.09.2014
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