0m o h NrhOet f h CG ehia Center. Technical CSG the of North-Ouest the to 10km approximatly located is site launch 6 Ariane The buildings. support and (BAL) building integration and assembly vehicle launch the (ZL4), pad launch the includes It activities. launch final the and vehicle launch with integration composite upper areathe preparation, dedicated final vehicle a launch for is designed (ELA-4) site launch 6 Ariane The A newlaunchingcomplex Arianespace family and its two next generation launch vehicles. the in vehicles three the of any using customers of needs the meet facilities preparation the tempo, launch high and capability launch multiple rockets’ the support to Designed infrastructure. commodious and clean-rooms vast to spacecrafts from different customers simultaneously, thanks several processing of capable are facilities space The the industry. in quality high their for recognized are that Facilities Preparation Payload modern provides CSG The State-of-the-art facilities other launchsites. most at Earth’s than here greater is the that effect slingshot a to – rotation due energy of boost extra an provides equator the to proximity its latitude, North degrees 5 at Located time. any at orbit any to payload any launching for conditions ideal offers (CSG) Center Space Guiana The Ideal location SPACEPORT THE WORLD’S under theITARregulation. governing the export of U.S. manufactured satellites or parts Specifically, the security regime is compliant with requirements to spacecraft. access limit strictly and Vega, and Soyuz, 5, Ariane systems: launch three the to apply They requirements. international and national both satisfy to authorities national of support the with implemented are measures rigorous and strict very sensitive ones by the French governement and consequently security highly as characterized are activities Arianespace and nationalagreementsrequirements. security measures that meet the most rigorous international The French government, the CSG, and Arianespace follow strict Strict security monitored. thoroughly are waste hazardous of disposal careful the and environment the on flight in vehicle launch the of impact The flight. and launch, preparation, spacecraft during measures strict through environment, the committed protecting been to have actors CSG all years, many For Environmental protection poised todealwithanyhazard. are teams response emergency and equipment safety that reported to the CSG responsible, bewhich in turn, makes to certain is activity dangerous potentially Any monitoring. operation permanent and certification, operator use, equipment of authorization includes this campaign: launch each during Rules Safety rigorous apply entities CSG The Safety mission

©Arianespace - Soyuz - September 2019 TECHNICAL OVERVIEW SOYUZ SOYUZ 1045 1045 Fairing Main Satellite 3343 3343

3529 Adapter ø3800 5060 Mini Satellite ø3800 (200-400 kg) The medium-lift Soyuz – which started operations from the Microsat Minisat H=1000 H=1500 Guiana Space Center (CSG) in 2011 and carried out more Micro Satellite 310 (<200 kg) L=1800 ø=1500 than twenty launches from French Guiana – is the industry’s l=800 longest-operating launcher with more than 1,900 manned and unmanned missions performed to date. Fregat Upper Stage Usable volume beneath payload Usable volume beneath Constellations launch Dual launch fairing and ASAP-S (Arianespace payload fairing configuration configuration Operated in concert with Ariane 5 and Vega, Soyuz from CSG System for Auxiliary Payloads) gives Arianespace the flexibility needed to orbit mid-sized Intermediate Bay satellites. Offering a payload capacity of 5 metric tons into low Earth orbit, or 3 metric tons into geostationary orbit, Soyuz at CSG is intended for the medium satellite market, including Earth observation, science missions and satellite constellation boom. Third Stage Restart capability and access to all orbits Ideal solution for launching constellations and multiple spacecraft The successful Soyuz at CSG program carries on a long- Fregat is an autonomous and flexible upper stage that extends standing collaboration between Europe and Russia, in Truss Interstage the capability of the lower three stages of the Soyuz vehicle to Thanks to a large variety of available dispensers, adapters particular commercial launches of Soyuz from Baikonur, provide access to a full range of orbits (LEO, SSO, MEO, GTO, and specific carrying structures, Soyuz can carry up to managed by the Starsem joint venture since 1996. The three GEO and escape). The stage can be restarted up to 6 times in 36 spacecraft and auxiliary passengers, thus making it a great Second Stage launch pads, in Baikonur, Vostochny and at CSG, are operated flight, thus enabling it to carry out complex mission profiles. solution for satellite constellations. concurrently, for the greatest benefit of Arianespace’s governmental and commercial customers. Payload fairing for a full range of spacecraft Back-up capabilities for 3-ton-class satellites The Soyuz currently offered by Arianespace is a four-stage passengers launch vehicle. The vehicle consists of four boosters (first The advent of Soyuz launches at CSG provides additional stage), a central core (second stage), a third stage, and the The Soyuz fairing has a diameter of 4.11 meters and an capacity to adjust the launch offering for geostationary restartable Fregat upper stage (fourth stage). Each vehicle also overall length of 11.4 meters – enabling it to accommodate satellites. The Arianespace back-up policy allows the 3-ton- includes a payload adapter/dispenser and fairing. the full range of payloads in the launch vehicle’s performance class satellites to be launched either on Ariane 5 in a dual category. launch configuration or on Soyuz as a dedicated launch. Unsurpassed flexibility Therefore, Arianespace increases the flexibility of its offer and the added value for the customer. The Soyuz is a reliable, efficient, and cost effective solution First Stage Boosters for a full range of missions from LEO to Mars. In its Soyuz mission profile for multiple launch in a circular orbit unequalled flight history, the Soyuz has already performed almost every mission profile, including orbiting satellites for telecommunications, Earth observation, weather monitoring, scientific missions and manned flights. It is a highly responsive ASAP-S upper part separation Mini-satellite and flexible launch vehicle. separation Fourth Fregat burn

First Fregat burn Third Fregat Performance GTO SSO LEO MEO HEO Earth escape burn

Transfer orbit Payloads, kg (including adapters) 3,250 4,400 4,850 1,645 2,250 2,000 Liftoff and ascent phase Mini-satellite separation orbit Inclination (i), deg 6 52 56

Altitude of perigee (Zp), km 250 820 920 23,222 Intermediate orbit

Altitude of apogee (Za), km 35,950 920 23,222 800,000

4 micro-satellites Argument of perigee (Wp), deg 178 separation Main-satellite separation orbit

Main-satellite separation Second Fregat burn