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41. http://www.cosmoworld.ru/spaceencyclopedia/publications/mks_eng.pdf
The Integrated Information Display System for the Soyuz-TMA and the Integrated Console of Manual Control Loop for the Russian Segment of the International Space Station Yurii Tiapchenko, deputy Chief Designer and head of the Division of Onboard Information Display Systems (1993-2002) at the Specialized Experimental Design Bureau of Spacecraft Technology and Chief Designer at the NTC "Alpha-M". ... The tasks of the spaceship IDS are provided by the Simvol and KL-110 display systems. ...
[ Текст ]  Ссылки http://www.cosmoworld.ru/spaceencyclopedia/publications/mks_eng.pdf -- 470.5 Кб -- 17.08.2005
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42. Second Spectrum-RG/eROSITA Conference
... Main Committees Venue Visa Accommodation Cultural program Information . ... If you travel alone, the cheapest option (saves you $30) is to obtain a "business visa" using an official invitation from KFU. If you travel with family members or need faster processing, you should obtain a "tourist visa". ... Most people travel to Russia on tourist visas. ... First eROSITA International Conference: Mapping the Structure of the Energetic Universe 17-20 Oct 2011, Garmisch-Partenkirchen (Germany) . ...
[ Сохраненная копия ]  Ссылки http://hea.iki.rssi.ru/kazan2012/index.php?p=visa -- 13.6 Кб -- 28.02.2014
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43. http://www.ssau.ru/files/science/conferences/itnt2015/itnt_2015_70.pdf
TOOLS OF TEST GENERATION FOR SATELLITES CONTROL PROGRAMS Andrey Tyugashev, Ekaterina Myasnikova, Elena Sopchenko S.P. Korolyov Samara State Aerospace University (National Reseach University) The paper presents a research in the field of test automation for testing spacecraft control programs. ... Programmers or designers of spacecraft systems write tests manually. ... Tests are carried out by issuing the control actions on the spacecraft and condition monitoring systems parameters of the spacecraft. ...
[ Текст ]  Ссылки http://www.ssau.ru/files/science/conferences/itnt2015/itnt_2015_70.pdf -- 161.6 Кб -- 04.08.2015
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44. Parameters of the Moon-perturbed orbit
... Parameters of the Moon-perturbed orbit . ... From orbits consistent with this limitation and with the date of the launch October 1, 2000 as an example, an orbit was selected with apogee directed to the North Galactic pole at the begining and rotation of orbit plane was maximized. The initial state vector is given in the inertial coordinate system in epoch J2000.0. ... The orbit has initial perigee radius Rp=7000.0 km, initial apogee radius Ra=343000.0 km and initial period T=8.453 days. ...
[ Сохраненная копия ]  Ссылки http://www.asc.rssi.ru/RadioAstron/documents/memo/mar98/memo_mar98.htm -- 5.4 Кб -- 05.10.1999
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45. Lunar equatorial positions. Explanations for Computer Ephemeris.
. Computer Ephemeris. Lunar equatorial positions. Explanations. Each row contains at 0 h and 12 h of Time Dynamical Terrestrial: month, day, apparent right ascension (hours, minutes, seconds), apparent declination (degrees, minutes, seconds of arc) and geocentric distance (in Earth's radii).
[ Сохраненная копия ]  Ссылки http://space.univ.kiev.ua/ephem/exp/Mo1.html -- 1.8 Кб -- 16.10.2004
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46. Vladimir Marsakov Abstracts
... The overall globular cluster population is divided by gap in the metallicity function at [Fe/H]=-1.0 into two discrete groups with well-defined maxima at [Fe/H]=-1.60?0.03 dex, and -0.60?0.04 dex. ... Clusters with extremely blue horizontal branches occupy a spherical volume of radius ~ 9 kpc, have high rotational velocities ( V rot =77?33 km/s), have substantial and equal negative radial and vertical metallicity gradients, and are, on average, the oldest group (the old-halo subsystem). ...
[ Сохраненная копия ]  Ссылки http://ip.rsu.ru/~marsakov/abs/abst29.htm -- 9.2 Кб -- 02.02.2007
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47. http://vast.sai.msu.ru/lk/
Please enter the lightcurve file name and period search parameters: . Lightcurve file: . ... Apply the Heliocentric correction and convert all dates to Terrestrial Time (TT)? ... Phase range for plots: -0.5 to 1.0 0.0 to 2.0 0.0 to 1.0 . ... Also, the Heliocentric correction cannot be applied to such lightcurves. ... Two period search methods are currently implemented. ... This period search service is also available at the mirror sites: Mirror 1 , Mirror 2 , Mirror 3 , Mirror 4 . ...
[ Сохраненная копия ]  Ссылки http://vast.sai.msu.ru/lk/ -- 6.4 Кб -- 18.08.2015
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48. SPUTNIK home page
... 0,50-0,59 (0,50-0,59) µm . ... Swath Width . ... at end of visibilty area . ... Visibility Area Width . ... Ground Resoultion in Nadir: . along swath . ... across swath . ... Ground Resolution at End of Visibilty Area: . ... 200 lines per second . ... at least 200 . Ground resolution corresponds to normal flihgt altitude 650 km. For more information send a mail to: info@sputnik.infospace.ru . ...
[ Сохраненная копия ]  Ссылки http://sputnik.infospace.ru/resurs/engl/msue_e.htm -- 8.3 Кб -- 21.01.2002
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49. http://www.wdcb.ru/stp/data/Images_of_f-plots/TABL/2003/aENGreadT.me.doc
FORMAT File Name : 1-3 Stations Code 4,5 Parameters Code 6,7 2 touches 8-11 Year 12-13 Month 14 A-The first half of table B-The second half of table Parameters and their Codes : foF2 -00 h' E -24 fxF2 -01 M3000F2 -03 fo Es -30 h'F2 -04 fb Es -32 foF1 -10 h' Es -34 M3000F1 -13 Type Es -36 h' F1 -14 f min -42 h' F -16 fxI -51 fo E -20 F spread -98 Thus- MGD42--200102A correspond to obs.Magadan,, F min, 2001 year, Februaey, The first half of table.
[ Текст ]  Ссылки http://www.wdcb.ru/stp/data/Images_of_f-plots/TABL/2003/aENGreadT.me.doc -- 22.0 Кб -- 21.11.2005
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50. University Satellites and Space Science Education '2006
University Satellites and . Space Science Education . ... Simulation of Code and Doppler GPS & GLONASS Observables and Feasible Positioning Algorithms for Universitetskiy-Tatyana Satellite . ... Algorithms of complex processing can give more accurate navigational results than algorithms which use observables of GPS only or GLONASS only. ... The algorithm of the modeling of observables has several steps. ... Skobeltsyn Institute of Nuclear Physics, Moscow State University, 2005-2006 . ...
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