Russian SHAREABLE DATA CENTER Institute of Solar-Terrestial Physics SB RAS . ... The ionogram catalogue is divided into the data file and the key file. ... The station codes database consists of the data file and two key files. ... This database consists of the data file and the key file. ... The antenna DB consists of two interrelated databases. ... The data file contains the following information: antenna type, antenna name, antenna parameters names, measurement units, and ranges of parameters. ...

... Master . ... Participants . ... Zel'dovich asteroid . ... YaB-100 conferences . ... Gnedin Yu.N. Investigation of vacuum polarization in strong magnetic fields of neutron stars: Zel'dovich ideological impetus . ... Doroshkevich A.G. Beyond the limits of the LambdaCDM cosmology . ... Illarionov A.F. Title is discussed . ... Imshennik V.S. Title is discussed . ... Polnarev A.G. Polarization of CMB generated by Cosmological Gravitational Waves . ... Ruzmaikin A.A. A game of chance . ...

... 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 . ...

... The OC "Mir" orbit parametres before the final burns . ... Orbit period (in min) . ... Mean orbit altitude (km) . ... solar F 10.7 flux . ... F 10.7 <= 100 - low level; 100 < F 10.7 < 150 - medium level; F 10.7 >= 150 - high level . Orbit 86328(15) - the first burn bulding the descent orbit  D V 1 =9.3 m/s. After burn altitude H min = 188.2 km, H max = 219.2 km. Orbit 86329(16) - the descent orbit second impulse D V 2 =10.4 m/s. After burn altitude H min = 158.9 km, H max = 218.5 km. ...

... ctronic modules Detectors unit . Bicounter module . ... The base of the electronics design is the same as in original MASS: modular structure, data exchange via RS485 interface, PMTs as light detectors. ... Detailed design of the MASS electronic modules (circuit diagrams, printed circuit b oard views, their sp ecifications) is provided in the second Chapter. ... SS MOSI 6 VCC GND LINE A OVLIGHT LINE B STROB 12 13 Figure 2.2: Circuit diagram of the analog part of the Bicounter module electronics. ...

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AAL Guestbook . Please Sign Our Guestbook . ... Previous Page | ... Signed on Thursday, March 17, 2005 at 15:11:05 CET . ... There's a great new astrobiology blog, run by newspaper editor Rob Bignell, at http://alienlifeblog.blogspot.com/. ... Signed on Saturday, December 25, 2004 at 02:46:35 CET . ... auch auf diesen Seiten . ... You have great designs on your site! ... Signed on Wednesday, December 22, 2004 at 17:38:52 CET . ... Signed on Thursday, October 28, 2004 at 19:39:53 CET . ...

... 1.1. ... re = mec 2 re. re=2.82ћ10-13 . ... 299.7925 300 -- : -12 -12 1 = 1.602192ћ10 1.6ћ10 . ... 12 1.602192 10 (/) - -- - () (e-) (e+): e- + e+ . ... 0 (4) : 1/2 (1.2) 4e2 N e 0 = = 5.64 10 me 4 N e ( -3 ) -1. . ... 2.5) E~m 2 eV0 = me e 4 2 = 27.21165 27.2 -- . ... 2.5) me c : (2.6) 2Ry = me c 2 me e4 e4 = 2 2 = 2 10-4. 2 c me c 2 , . ... t=1/, meV 2 t ~ . ... re e 2 mee 2 e4 = 2 = 2 2 = 2. a0 mec 2 c , (2.6). , . ... t0 = a0 V0 = 3 me e 4 2.5 10 -17 , 0 = 1 me e4 = 3 4.11016 c-1 , t0 , . ...

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SITE 2010 Comprehensive Characterization of Astronomical Sites Kislovodsk, Russia, 49 October 2010 Conference Summary Marc S. Sarazin*a a European Southern Observatory, Garching, Germany Abstract The main topics discussed during the Site 2010 conference are outlined and the outcome is described. Keywords: Astronomical Site testing, precipitable water vapor, atmospheric turbulence, cloudiness, seeing 1. ... Site surveys for National observatory projects in China, India, and Iran benefit from this. ...

Multipurpose Aerospace System (MAKS) . ... Up to date the main components of the orbital stage construction have been worked up, external fuel tank mock-up has been made, significant work has been already done on the propulsion system MAKS consists of the subsonic carrier aircraft and an orbital stage with an external fuel tank mounted on it As the first stage the An-225 MRIA aircraft originally intended for the BURAN transportation is used. ... CREATION AIRFRAME OF THE BURAN ORBITAL SPACESHIP . ...