FOC-M5 (Launch in October 2016, Ariane-5)• FM10 at ESTEC. TVAC completed• FM11 at ESTEC. Starting environmental test campaign• FM12 at OHB Bremen, completing integration activities• FM7 at OHB Bremen, completing integration activities
From a recent presentation made by ESA representative (Guenter Hein) on IAIN 2015 conference:QuoteFOC-M5 (Launch in October 2016, Ariane-5)• FM10 at ESTEC. TVAC completed• FM11 at ESTEC. Starting environmental test campaign• FM12 at OHB Bremen, completing integration activities• FM7 at OHB Bremen, completing integration activities
This has been slipped into November 2016.
In the autumn of this year, four Galileos will be launched together for the very first time, on a specially customised launcher, called the Ariane 5 ES Galileo.In development since 2012, this new launcher variant has evolved from the Ariane 5 ES (Evolution Storable), used to place ESA’s 20 000 kg ATV supply vehicle into low-Earth orbit.This launder has to carry a lower mass payload – four fully fuelled 738 kg Galileo satellites plus their supporting dispenser – but needs to take it up to the much higher altitude of medium-Earth orbit, approximately 23 222 km up.
Quote from: beidou on 06/14/2016 07:33 pmIn the autumn of this year, four Galileos will be launched together for the very first time, on a specially customised launcher, called the Ariane 5 ES Galileo.In development since 2012, this new launcher variant has evolved from the Ariane 5 ES (Evolution Storable), used to place ESA’s 20 000 kg ATV supply vehicle into low-Earth orbit.This launder has to carry a lower mass payload – four fully fuelled 738 kg Galileo satellites plus their supporting dispenser – but needs to take it up to the much higher altitude of medium-Earth orbit, approximately 23 222 km up.Other than the Galileo dispenser, any body know what's different with Ariane 5 ES Galileo compared to the standard Ariane 5 ES?
Other than the Galileo dispenser, any body know what's different with Ariane 5 ES Galileo compared to the standard Ariane 5 ES?
Furthermore, in order to address the mission’s performance requirements (four satellites each weighing 738kg, or about 3 tonnes, into a 29,300km orbit inclined at 56° ± 2°), the mass of the upper composite had to be reduced. Marie-Paule explains: “The only component on which significant mass savings could be achieved was the structure of the vehicle equipment bay, the ‘brain’ of Ariane 5. Designed for the ATV, the bay was over-sized for the Galileo mission. This structure has therefore been optimised in terms of mass, based on the specific context of the Galileo mission.”