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181. New Page 11
... This is commonly referred to as CPM (cost per thousand impressions).We pay you a percentage of revenues for the ads that you and your friends view with Harry, based on current CPM rates.You will get 75% of total revenue generated from your viewing.. ... REMEMBER: for every one hour the program on Your screen You'll get paid $0.50. And when You recommend those program to Your friends, reffering to Your personal ID, You'll get paid $0.10 for every hour the program open on Your's friends computer. ...
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Ссылки http://sitilia.chat.ru/newpage11.htm -- 20.1 Кб -- 09.04.2016
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182. http://www.tunguska.ru/nc/nlc-luna/Schroeder_comments.pdf
Journal of Atmospheric and Solar-Terrestrial Physics Manuscript Draft Manuscript Number: ATP1021 Title: comment on the paper by Dalin , Pertsev and Romejko Significance of lunar impact on noctilucent clouds ( revised version) Article Type: Research Paper Section/Category: Keywords: Noctilucent clouds moon influence mesosphere Manuscript Region of Origin: Abstract: a critical review of the paper by Dalin , ... Reference: Dalin, P.A., N.N. Pertsev, V.A. Romejko. ...
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Ссылки http://www.tunguska.ru/nc/nlc-luna/Schroeder_comments.pdf -- 202.9 Кб -- 19.11.2010
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183. http://xmm.vilspa.esa.es/sas/5.4.1/doc/saslib/rfc1321.txt
... April 1992 The MD5 Message-Digest Algorithm Status of this Memo This memo provides information for the Internet community. ... combination): -sstring - digests string -t - runs time trial -x - runs test script filename - digests file (none) - digests standard input */ int main (argc, argv) int argc; Rivest [Page 17] RFC 1321 MD5 Message-Digest Algorithm April 1992 char *argv[]; { int i; if (argc 1) for (i = 1; i argc; i++) if (argv[i][0] == '-' argv[i][1] == 's') MDString (argv ...
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Ссылки http://xmm.vilspa.esa.es/sas/5.4.1/doc/saslib/rfc1321.txt -- 35.4 Кб -- 06.04.1993
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184. 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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