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A navigational box that can be placed at the bottom of articles. Template parameters [Edit template data] Parameter Description Type Status State state The initial visibility of the navbox Suggested values collapsed expanded autocollapse String suggested Template transclusions Transclusion maintenance Check completeness of transclusions The above documentation is transcluded from Template ...
The AMOS bus is a lightweight version used for satellites between 1.5 and 2 t (1.7 and 2.2 tons), with 800 to 1700 watts of power. [3] [4] [5] The satellite bus started with the AMOS-1, the smallest of all the family, and increased mass, payload successively in the AMOS-2 and AMOS-3.
AMOS-2 carries 28 Ku-band transponders; twenty-two active with six as backups. [4] With a mass of 1370 kg at launch, AMOS-2 incorporated a 400 newtons liquid apogee boost motor and fourteen 10 newtons reaction control thrusters for raising the satellite's orbit from geostationary transfer orbit (GTO) to its final geostationary orbit as well as for its attitude control.
AMOS ("Affordable Modular Optimized Satellite") is a series of Israeli communications satellites operated by Israel-based Spacecom.All AMOS satellites were developed by Israel Aerospace Industries (IAI) using the AMOS bus satellite bus, except for AMOS-5 which was developed by ISS Reshetnev using the Ekspress bus satellite bus, and AMOS-17 which was developed by Boeing on its BSS-702.
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The satellite is powered by twin solar panels, and is based on the Israeli AMOS Bus. It replaced AMOS-1 in geosynchronous orbit at 4° West. AMOS-3 carries fourteen Ku-band / Ka-band transponders, and is expected to have an on-orbit lifetime of 18 years.
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AMOS-1 and AMOS-2 were placed near each other to enable satellite users to aim once and reach either satellite from the same antenna. [4] Launch was insured for over US$145 million. The satellite AMOS-1 was operational on 1 July 1996.
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