... a = 0: MM seed 10 2 M , z s = 20 В 30 ; a = 0.95 : MM seed 103 M , zs = 20 В 30 ; ; (merging), ?! a = 1.0 : MM seed 105 M , zs > 20 a* = 0.998 J0836+0054 = 0.32 z = 5.810 LEdd = 2.6 в1047 erg / s M BH = 9.3 в 109 M L j = 3.9 в1049 erg / s J1030+0524 M ...
... of NEAs orbital resonance mo tions by numerical methods --- 20 min O. M. Kochetova ... orbits with the e#ects of luni--solar perturbations --- 20 min S. M. Kudryavtsev ...
... 15.20 - |M. A. Sadovnikov, A. L. Sokolov, N. M. Souzova (OJC «RPC | | |«Precision Systems and Instruments», Moscow, Russia) | ... 10.20 - |traffic control of space debris based on a 3 m telescope. ...
... соединения h m s Солнца и Луны по прямому восхождению 2012, май 20, 23 59 09.2 ... h m Ѓ Ѓ Ѓ Ѓ Ѓ Ѓ Ѓ њ ' 20 50 ... m sЃ Ѓ њ 22 10 Ў+24 19.3Ѓ+120 08.7Ў+23 47.2Ѓ+115 21.0Ў ЂЂЂ Ѓ ЂЂЂ Ў 4 26 Ѓ ЂЂ Ѓ 6.9 ...
... Measurements of turbulent strength along the path Cn , 2 -2/ 3 ( ( ( ( 08.09.09 1 1 :5 1 With heating Cn2 = (4-20-170)*10 m -14 -2/3 ( ( Without heating Cn2 = (2-5-7)*10-14m -2/3 , Detection of illumination concentration on remote target Active action on ...
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Ссылки http://www.ipa.nw.ru/conference/wpltn2012/docs/27/1100%20Nonlinear-optical%20Approach.pdf -- 612.1 Кб -- 01.10.2012 Похожие документы
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