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It utilises a chemical, bi-propellant propulsion system for orbit raising and on-station manoeuvres with an optional plasma propulsion system PPS. The Eurostar E satellite model currently [ when?
They have just become larger, more powerful, with implementation costs reduced through longer orbit manoeuvring lifetime, and more efficient and powerful payloads.
The Eurostar satellite structures are modular with a separate Service-Propulsion module and Communications module. Please update this article to reflect recent events or newly available information.
Eurostar (satellite bus)
This system is most commonly used for North-South station-keeping. A new version Ee introduced in uses electric propulsion for orbit raising. Spacecraft stubs Satellite buses.
This was the first commercial satellite to have a digital avionics system modular in concept.
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Retrieved October 1, It is a member of Airbus Kicronet and Space’s Eurostar family. Nowadays the Eurostar E series has been considerably enhanced and updated with the latest technologies, still maintaining the basic proven configuration. Satellite payload power was from to W. The E was the first commercial satellite family to use lithium-ion batteries rather than the older nickel-based technologies for power supply during eclipses.
In March Airbus Defence and Space received micrpnet delivery of new 3D printed brackets for mounting Telemetry and Tele-Command antennas, being the first space-qualified 3D printed component of its kind. This page was last edited on 12 Marchat Please help improve this article by adding citations to reliable sources. Telstar 12 Vantage . They tend to feature between 50 and microndt transponders, most often in the K u band and C band.
Use British English from January Use dmy dates from August Wikipedia articles in need of updating from August All Wikipedia articles in need of updating All stub articles. In Decemberthe Eurostar satellites accumulated years of successful operations in orbit.
Retrieved 6 February Eurostar was designed in the mid s jointly by Matra Marconi Space and BAe under the “United Satellite” venture, now integrated within Airbus Defence and Space to an internally developed specification,  for a market which at the time had a design envelope of 1.
All articles with dead external links Articles with dead external links from November Articles with permanently dead external links Articles needing additional references from February All articles needing additional references All articles with vague or ambiguous time Vague shuytle ambiguous time from July All articles with unsourced statements Articles with unsourced statements from July Use British English from January The PPS harnesses the Newtonian effect as a result of the ionisation of xenon gas employed by the shuttlle of Hall effect plasma thrusters.
With this system architecture, all key satellite parameters are in software, which permits mission specific requirements to be implemented without hardware changes. Views Read 3000d View history.