... Ыагл Ыи жи гв зи гв кг в ДЪ О НЕ cw nd = cw nd rwnd FlightSize ssthresh SMSS Й i RTO min(cwnd , rwnd ) - FlightSize ? ... Ыагл Ыи жи гв зи гв кг в ssthresh max (FlightSize /2, 2 SMSS ) cwnd Й R TO И И И И SMSS ssthresh max (FlightSize /2, 2 SMSS ) max (FlightSize /2, IW = cwnd0 ) cwnd Й ЪЬЧ ДЪ ПЕ И в Тг R TT И И К SRTT = (ALPHA SRTT ) + ((1 - ALPHA) RTT ) Э ЧЭЦ Д И Н ЕИ Ф ЧЭЦ Н ЕИ ФШР Ь RTO = min[UBOUND , max [LBOUND , (BETA SRTT )]] Д Д Д Й И И МК ЕИ И ОКМЕК ж Ян ? ...

... NASA Lunar Orbiter . ... The Lunar Prospector is designed for a low-polar orbit investigation of the Moon, including mapping of surface composition and possible polar ice deposits, measurements of magnetic and gravity fields, and study of lunar outgassing events. Data from the 1- to 3-year mission will allow construction of a detailed map of the surface composition of the Moon, and will improve our understanding of the origin, evolution, current state, and resources of the Moon. ...

Cosmic Research, Vol. 42, No. 5, 2004, pp. 435­488. Translated from Kosmicheskie Issledovaniya, Vol. 42, No. 5, 2004, pp. 453­508. Original Russian Text Copyright © 2004 by Veselovsky, Panasyuk, Avdyushin, Bazilevskaya, Belov, Bogachev, Bogod, Bogomolov, Bothmer, Boyarchuk, Vashenyuk, Vlasov, Gnezdilov, Gorgutsa, Grechnev, Denisov, Dmitriev, Dryer, Yermolaev, Eroshenko, Zherebtsov, Zhitnik, Zhukov, Zastenker, Zelenyi, Zeldovich, Ivanov-Kholodnyi, Ignat'ev, Ishkov, Kolomiytsev, Krasheninnikov, Kudela,