... The PROTON launcher injected the satellite into a transfer orbit and INTEGRAL's own propulsion system brought the satellite into its 72 hours eccentric operational orbit with an apogee of 153600 km and an inclination of 52.5 degrees. ...
... The PROTON launcher injected the satellite into a transfer orbit and INTEGRAL's own propulsion system brought the satellite into its 72 hours eccentric operational orbit with an apogee of 153600 km and an inclination of 52.5 degrees. ...
... This research has made use of data obtained from NED (Jet Propulsion Laboratory, California Institute of Technology), SIMBAD (CDS, Strasbourg, France) and HEASARC (NASA's Goddard Space Flight Center). t Figure 1. ...
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Ссылки http://hea.iki.rssi.ru/integral06/papers/D30_Malizia01-19Jan07_18:12:36.pdf -- 545.4 Кб -- 19.01.2007 Похожие документы
... Tony Mroczkowski (California Institute of Technology/Jet Propulsion Lab, Pasadena, USA) High-Resolution SZE Confirmation of ... Dr. Mro czkowski, Tony, California Institute of Technology/Jet Propulsion Lab, Pasadena, USA tonym@astro.caltech.edu 75. ...
... To achieve the proper reference orbit from the Baikonur launch site an additional boost with a characteristic velocity of ~260 m/s is performed igniting the booster's propulsion unit. ...
... This research has made use of data obtained from NED (Jet Propulsion Laboratory, California Institute of Technology), SIMBAD (CDS, Strasbourg, France) and HEASARC (NASA's Goddard Space Flight Center). ...
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Ссылки http://hea.iki.rssi.ru/integral06/papers/D01_Bassani01-22Jan07_16:19:17.pdf -- 235.4 Кб -- 22.01.2007 Похожие документы
... This research has made use of the NASA/IPAC Extragalactic Database (NED) which is operated by the Jet Propulsion Laboratory, of data obtained from the High Energy Astrophysics Science Archive Research Center (HEASARC), provided by NASA's Goddard Space ...
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Ссылки http://hea.iki.rssi.ru/integral06/papers/D02_Beckmann01-19Jan07_20:50:38.pdf -- 156.2 Кб -- 19.01.2007 Похожие документы