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55-545: The satellite was successfully launched into space on May 4, 2017, at 21:52 UTC, by means of an Ariane 5 vehicle from the French company Arianespace , launched from Guiana Space Centre , Kourou , French Guiana , together with the Koreasat 7 . It had a launch mass of 12,800 pounds (5,800 kg). The SGDC will be equipped with 50 Ka band transponders and 5 X band transponders to provide broadband internet and communications to

110-509: A SYLDA ( Système de Lancement Double Ariane , meaning "Ariane Double-Launch System") carrier system. Up to three, somewhat smaller, main satellites are possible depending on size using a SPELTRA ( Structure Porteuse Externe Lancement Triple Ariane , which translates to "Ariane Triple-Launch External Carrier Structure"). Up to eight secondary payloads, usually small experiment packages or minisatellites , could be carried with an ASAP (Ariane Structure for Auxiliary Payloads) platform. Following

165-425: A 5.4 m (18 ft) diameter by 30.5 m (100 ft) high tank with two compartments, one for liquid oxygen and one for liquid hydrogen , and a Vulcain 2 engine at the base with a vacuum thrust of 1,390 kN (310,000 lb f ). The H173 EPC weighed about 189 t (417,000 lb), including 175 t (386,000 lb) of propellant. After the main cryogenic stage runs out of fuel, it re-entered

220-487: A European launch vehicle, providing supplies to the space station with necessary propellant, water, air and dry cargo. This was the first operational Ariane mission which involved an engine restart in the upper stage. The ES-ATV Aestus EPS upper stage was restartable while the ECA HM7-B engine was not. On 1 July 2009, an Ariane 5ECA launched TerreStar-1 (now EchoStar T1), which was then, at 6,910 kg (15,230 lb),

275-498: A commercial record, lifting Yahsat 1A and Intelsat New Dawn with a total payload weight of 10,064 kg (22,187 lb) to transfer orbit. This record was later broken again during the launch of Ariane 5ECA flight VA-208 on 2 August 2012, lifting a total of 10,182 kg (22,447 lb) into the planned geosynchronous transfer orbit, which was broken again 6 months later on flight VA-212 with 10,317 kg (22,745 lb) sent towards geosynchronous transfer orbit. In June 2016,

330-404: A design might not have been possible if the higher Max-Q for the launch of this launch vehicle would have posed a constraint on the mass delivered to orbit. The design brief of the next generation launch vehicle Ariane 6 called for a lower-cost and smaller launch vehicle capable of launching a single satellite of up to 6,500 kg (14,300 lb) to GTO. However, after several permutations

385-584: A direct successor system, first launched in 2024. The system was designed as an expendable launch vehicle by the Centre national d'études spatiales (CNES), the French government's space agency, in cooperation with various European partners. Despite not being a direct derivative of its predecessor launch vehicle program, it was classified as part of the Ariane rocket family . Aérospatiale , and later ArianeGroup ,

440-591: A new commercial payload lifting record of 8,200 kg (18,100 lb). The dual-payload consisted of the Thaicom 5 and Satmex 6 satellites. On 4 May 2007, the Ariane 5ECA set another new commercial record, lifting into transfer orbit the Astra 1L and Galaxy 17 communication satellites with a combined weight of 8,600 kg (19,000 lb), and a total payload weight of 9,400 kg (20,700 lb). This record

495-562: A payload of 7,639 lb (3,465 kg) to the same orbit. Solid propellant boosters are not controllable and must generally burn until exhaustion after ignition, unlike liquid propellant or cold-gas propulsion systems. However, launch abort systems and range safety destruct systems can attempt to cut off propellant flow by using shaped charges . As of 1986 estimates for SRB failure rates have ranged from 1 in 1,000 to 1 in 100,000. SRB assemblies have failed suddenly and catastrophically. Nozzle blocking or deformation can lead to overpressure or

550-462: A reduction in thrust, while defects in the booster's casing or stage couplings can cause the assembly to break apart by increasing aerodynamic stresses. Additional failure modes include bore choking and combustion instability. Failure of an O-ring seal on the Challenger space shuttle's right solid rocket booster led to its disintegration shortly after liftoff. Solid rocket motors can present

605-405: A relatively simple design. They provide greater thrust without significant refrigeration and insulation requirements, and produce large amounts of thrust for their size. Adding detachable SRBs to a vehicle also powered by liquid-propelled rockets known as staging reduces the amount of liquid propellant needed and lowers the launch rig mass. Solid boosters are cheaper to design, test, and produce in

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660-571: A telemetry loss occurred between the launch vehicle and the ground controllers. It was later confirmed, about 1 hour and 20 minutes after launch, that both satellites were successfully separated from the upper stage and were in contact with their respective ground controllers, but that their orbital inclinations were incorrect as the guidance systems might have been compromised. Therefore, both satellites conducted orbital procedures, extending commissioning time. SES-14 needed about 8 weeks longer than planned commissioning time, meaning that entry into service

715-785: A third burn after ATV deployment to de-orbit the stage. This procedure was repeated for all subsequent ATV flights. Ariane 5ECA used the ESC ( Étage Supérieur Cryotechnique — Cryogenic Upper Stage), which was fueled by liquid hydrogen and liquid oxygen. The ESC used the HM7B engine previously used in the Ariane 4 third stage. The propellent load of 14.7 tonne allowed the engine to burn for 945 seconds while providing 6.5 tonne of thrust. The ESC provided roll control during powered flight and full attitude control during payload separation using hydrogen gas thrusters. Oxygen gas thrusters allowed longitudinal acceleration after engine cutoff. The flight assembly included

770-657: Is a retired European heavy-lift space launch vehicle operated by Arianespace for the European Space Agency (ESA). It was launched from the Guiana Space Centre (CSG) in French Guiana . It was used to deliver payloads into geostationary transfer orbit (GTO), low Earth orbit (LEO) or further into space. The launch vehicle had a streak of 82 consecutive successful launches between 9 April 2003 and 12 December 2017. Since 2014, Ariane 6 ,

825-460: The Ariane 4 where efficiency considerations (the computer running the software had an 80% maximum workload requirement ) led to four variables being protected with a handler while three others, including the horizontal bias variable, were left unprotected because it was thought that they were "physically limited or that there was a large margin of safety". The software, written in Ada , was included in

880-586: The Brazilian government and the Brazilian Armed Forces . A backup satellite, SGDC-2 , was initially planned for launch no earlier than 2022. As of July 2021, the procurement of this satellite has been delayed indefinitely due to concerns over cost and the legality of the procurement agreement. This article about one or more spacecraft of Brazil is a stub . You can help Misplaced Pages by expanding it . Ariane 5 Ariane 5

935-419: The Ariane 5 through the reuse of an entire Ariane 4 subsystem despite the fact that the particular software containing the bug, which was just a part of the subsystem, was not required by the Ariane 5 because it has a different preparation sequence than the Ariane 4. The second test flight (L502, on 30 October 1997) was a partial failure. The Vulcain nozzle caused a roll problem, leading to premature shutdown of

990-460: The Ariane 5ECA took place on 12 February 2005. The payload consisted of the XTAR-EUR military communications satellite, a 'SLOSHSAT' small scientific satellite and a MaqSat B2 payload simulator. The launch had been scheduled for October 2004, but additional testing and a military launch (of a Helios 2A observation satellite) delayed the attempt. On 11 August 2005, the first Ariane 5GS (featuring

1045-539: The Ariane 5ECA's improved solid motors) boosted Thaicom 4 , the heaviest telecommunications satellite to date at 6,505 kg (14,341 lb), into orbit. On 16 November 2005, the third Ariane 5ECA launch (the second successful ECA launch) took place. It carried a dual payload consisting of Spaceway F2 for DirecTV and Telkom-2 for PT Telekomunikasi of Indonesia . This was the launch vehicle's heaviest dual payload to date, at more than 8,000 kg (18,000 lb). On 27 May 2006, an Ariane 5ECA launch vehicle set

1100-539: The Ariane 5ME with total development effort expected to cost €1 billion. On 21 November 2012, ESA agreed to continue with the Ariane 5ME to meet the challenge of lower priced competitors. It was agreed the Vinci upper stage would also be used as the second stage of a new Ariane 6, and further commonality would be sought. Ariane 5ME qualification flight was scheduled for mid-2018, followed by gradual introduction into service. On 2 December 2014, ESA decided to stop funding

1155-465: The Ariane programme, but this was most likely an inference based on early blueprints of the Ariane 6 having a central P80 booster and 2-4 around the main one. The incorporation of the ESC-B with the improvements to the solid motor casing and an uprated Vulcain engine would have delivered 27,000 kg (60,000 lb) to LEO. This would have been developed for any lunar missions but the performance of such

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1210-679: The GTO record was raised to 10,730 kg (23,660 lb), on the first rocket in history that carried a satellite dedicated to financial institutions. The payload record was pushed a further 5 kg (11 lb), up to 10,735 kg (23,667 lb) on 24 August 2016 with the launch of Intelsat 33e and Intelsat 36 . On 1 June 2017, the payload record was broken again to 10,865 kg (23,953 lb) carrying ViaSat-2 and Eutelsat-172B . In 2021 VA-255 put 11,210 kg into GTO. On 25 January 2018, an Ariane 5ECA launched SES-14 and Al Yah 3 satellites. About 9 minutes and 28 seconds after launch,

1265-580: The Guiana Space Center for analysis. Prior to that mission, the last such recovery and testing was done in 2003. The French M51 submarine-launched ballistic missile (SLBM) shared a substantial amount of technology with these boosters. In February 2000, the suspected nose cone of an Ariane 5 booster washed ashore on the South Texas coast, and was recovered by beachcombers before the government could get to it. The second stage

1320-474: The Vehicle Equipment Bay, with flight electronics for the entire rocket, and the payload interface and structural support. The payload and all upper stages were covered at launch by a fairing for aerodynamic stability and protection from heating during supersonic flight and acoustic loads. It was jettisoned once sufficient altitude has been reached, typically above 100 km (62 mi). It

1375-501: The W3B satellite failed to operate shortly after the successful launch and was written off as a total loss due to an oxidizer leak in the satellite's main propulsion system. The BSAT-3b satellite, however, is operating normally. The VA253 launch on 15 August 2020 introduced two small changes that increased lift capacity by about 85 kg (187 lb); these were a lighter avionics and guidance-equipment bay, and modified pressure vents on

1430-481: The atmosphere for an ocean splashdown. Attached to the sides were two P241 (P238 for Ariane 5G and G+) solid rocket boosters (SRBs or EAPs from the French Étages d'Accélération à Poudre ), each weighing about 277 t (611,000 lb) full and delivering a thrust of about 7,080 kN (1,590,000 lb f ). They were fueled by a mix of ammonium perchlorate (68%) and aluminium fuel (18%) and HTPB (14%). They each burned for 130 seconds before being dropped into

1485-493: The core stage. The upper stage operated successfully, but it could not reach the intended orbit. A subsequent test flight (L503, on 21 October 1998) proved successful and the first commercial launch (L504) occurred on 10 December 1999 with the launch of the XMM-Newton X-ray observatory satellite. Another partial failure occurred on 12 July 2001, with the delivery of two satellites into an incorrect orbit, at only half

1540-557: The development of Ariane 5ME and instead focus on Ariane 6, which was expected to have a lower cost per launch and allow more flexibility in the payloads (using two or four P120C solid boosters depending on total payload mass). Work on the Ariane 5 EAP motors was continued in the Vega programme. The Vega 1st stage engine – the P80 engine – was a shorter derivation of the EAP. The P80 booster casing

1595-509: The failure of the first ECA flight in 2002, combined with a deteriorating satellite industry, caused ESA to cancel development in 2003. Development of the Vinci engine continued, though at a lower pace. The ESA Council of Ministers agreed to fund development of the new upper stage in November 2008. In 2009, EADS Astrium was awarded a €200 million contract, and on 10 April 2012 received another €112 million contract to continue development of

1650-619: The finalized design was nearly identical in performance to the Ariane 5, focusing instead on lowering fabrication costs and launch prices. As of March 2014 , Ariane 6 was projected to be launched for about €70 million per flight, about half of the Ariane 5 price. Initially development of Ariane 6 was projected to cost €3.6 billion. In 2017, the ESA set 16 July 2020 as the deadline for the first flight. The Ariane 6 successfully completed its maiden flight on 9 July 2024. Ariane 5's first test flight ( Ariane 5 Flight 501 ) on 4 June 1996 failed, with

1705-537: The first ECA launch was the last failure of an Ariane 5 until flight 240 in January 2018. On 27 September 2003, the last Ariane 5G boosted three satellites (including the first European lunar probe, SMART-1 ), in Flight 162. On 18 July 2004, an Ariane 5G+ boosted what was at the time the heaviest telecommunication satellite ever, Anik F2 , weighing almost 6,000 kg (13,000 lb). The first successful launch of

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1760-535: The height of the intended GTO. The ESA Artemis telecommunications satellite was able to reach its intended orbit on 31 January 2003, through the use of its experimental ion propulsion system. The next launch did not occur until 1 March 2002, when the Envisat environmental satellite successfully reached an orbit of 800 km (500 mi) above the Earth in the 11th launch. At 8,111 kg (17,882 lb), it

1815-508: The intended altitude, they had been programmed for the standard geostationary transfer orbit of 90° when the payloads were intended to be 70° for this supersynchronous transfer orbit mission, 20° off norme. This mission anomaly marked the end of 82nd consecutive success streak since 2003. Ariane 5 launch vehicles had accumulated 117 launches, 112 of which were successful, yielding a 95.7% success rate. Between April 2003 and December 2017, Ariane 5 flew 83 consecutive missions without failure, but

1870-541: The largest and most massive commercial telecommunication satellite ever built at that time until being overtaken by Telstar 19 Vantage , at 7,080 kg (15,610 lb), launched aboard Falcon 9 . The satellite was launched into a lower-energy orbit than a usual GTO, with its initial apogee at roughly 17,900 km (11,100 mi). On 28 October 2010, an Ariane 5ECA launched Eutelsat 's W3B (part of its W Series of satellites) and Broadcasting Satellite System Corporation (B-SAT)'s BSAT-3b satellites into orbit. But

1925-558: The launch of 15 August 2020, Arianespace signed the contracts for the last eight Ariane 5 launches, before it was succeeded by the new Ariane 6 launcher, according to Daniel Neuenschwander, director of space transportation at the ESA. Ariane 5 flew its final mission on 5 July 2023. Ariane 5's cryogenic H173 main stage (H158 for Ariane 5G, G+, and GS) was called the EPC ( Étage Principal Cryotechnique — Cryotechnic Main Stage). It consisted of

1980-491: The launch vehicle suffered a partial failure in January 2018. All launches are from Guiana Space Centre , ELA-3 . Solid rocket booster A solid rocket booster ( SRB ) is a large solid propellant motor used to provide thrust in spacecraft launches from initial launch through the first ascent. Many launch vehicles, including the Atlas V , SLS and Space Shuttle , have used SRBs to give launch vehicles much of

2035-496: The long run compared to the equivalent liquid propellant boosters. Reusability of components across multiple flights, as in the Shuttle assembly, also has decreased hardware costs. One example of increased performance provided by SRBs is the Ariane 4 rocket. The basic 40 model with no additional boosters was capable of lifting a 4,795 lb (2,175 kg) payload to geostationary transfer orbit . The 44P model with 4 solid boosters has

2090-755: The new Ariane 6 . With first flight planned for 2018, it would have become ESA's principal launcher until the arrival of the new Ariane 6 version. ESA halted funding for the development of Ariane 5ME in late 2014 to prioritize development of Ariane 6. The Ariane 5ME was to use a new upper stage, with increased propellant volume, powered by the new Vinci engine . Unlike the HM-7B engine, it was to be able to restart several times, allowing for complex orbital maneuvers such as insertion of two satellites into different orbits, direct insertion into geosynchronous orbit, planetary exploration missions, and guaranteed upper stage deorbiting or insertion into graveyard orbit . The launcher

2145-519: The ocean. The SRBs were usually allowed to sink to the bottom of the ocean, but, like the Space Shuttle Solid Rocket Boosters , they could be recovered with parachutes, and this was occasionally done for post-flight analysis. Unlike Space Shuttle SRBs, Ariane 5 boosters were not reused. The most recent attempt was for the first Ariane 5 ECA mission in 2009. One of the two boosters was successfully recovered and returned to

2200-567: The payload fairing, which were required for the subsequent launch of the James Webb Space Telescope. It also debuted a location system using Galileo navigation satellites . On 25 December 2021, VA256 launched the James Webb Space Telescope towards a Sun–Earth L 2 halo orbit . The precision of trajectory following launch led to fuel savings credited with potentially doubling the lifetime of

2255-416: The rocket self-destructing 37 seconds after launch because of a malfunction in the control software. A data conversion from 64- bit floating-point value to 16-bit signed integer value to be stored in a variable representing horizontal bias caused a processor trap (operand error) because the floating-point value was too large to be represented by a 16-bit signed integer. The software had been written for

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2310-411: The telescope by leaving more hydrazine propellant on board for station-keeping than was expected. According to Rudiger Albat, the program manager for Ariane 5, efforts had been made to select components for this flight that had performed especially well during pre-flight testing, including "one of the best Vulcain engines that we've ever built." On 22 April 2011, the Ariane 5ECA flight VA-201 broke

2365-517: The thrust required to place the vehicle into orbit. The Space Shuttle used two Space Shuttle SRBs , which were the largest solid propellant motors ever built and the first designed for recovery and reuse. The propellant for each solid rocket motor on the Space Shuttle weighed approximately 500,000 kilograms. Compared to liquid propellant rockets , the solid-propellant motors (SRMs) have been capable of providing large amounts of thrust with

2420-531: Was again broken by another Ariane 5ECA, launching the Skynet 5B and Star One C1 satellites, on 11 November 2007. The total payload weight for this launch was of 9,535 kg (21,021 lb). On 9 March 2008, the first Ariane 5ES-ATV was launched to deliver the first ATV called Jules Verne to the International Space Station (ISS). The ATV was the heaviest payload ever launched by

2475-430: Was also confirmed healthy after more than 12 hours without further statement, and like SES-14, Al Yah 3's maneuvering plan was also revised to still fulfill the original mission. As of 16 February 2018, Al Yah 3 was approaching the intended geostationary orbit, after series of recovery maneuvers had been performed. The investigation showed that invalid inertial units' azimuth value had sent the vehicle 17° off course but to

2530-417: Was also to include a lengthened fairing up to 20 m (66 ft) and a new dual launch system to accommodate larger satellites. Compared to an Ariane 5ECA model, the payload to GTO was to increase by 15% to 11,500 kg (25,400 lb) and the cost-per-kilogram of each launch was projected to decline by 20%. Originally known as the Ariane 5 ECB , Ariane 5ME was to have its first flight in 2006. However,

2585-409: Was capable of repeated ignition, first demonstrated during flight V26 which was launched on 5 October 2007. This was purely to test the engine, and occurred after the payloads had been deployed. The first operational use of restart capability as part of a mission came on 9 March 2008, when two burns were made to deploy the first Automated Transfer Vehicle (ATV) into a circular parking orbit, followed by

2640-526: Was lost in the Atlantic Ocean . The fault was determined to have been caused by a leak in coolant pipes allowing the nozzle to overheat. After this failure, Arianespace SA delayed the expected January 2003 launch for the Rosetta mission to 26 February 2004, but this was again delayed to early March 2004 due to a minor fault in the foam that protects the cryogenic tanks on the Ariane 5. The failure of

2695-419: Was made by Ruag Space and since flight VA-238 it was composed of 4 panels. As of November 2014 , the Ariane 5 commercial launch price for launching a "midsize satellite in the lower position" was approximately €50 million, competing for commercial launches in an increasingly competitive market . The heavier satellite was launched in the upper position on a typical dual-satellite Ariane 5 launch and

2750-468: Was made of filament wound graphite epoxy, much lighter than the current stainless steel casing. A new composite steerable nozzle was developed while new thermal insulation material and a narrower throat improved the expansion ratio and subsequently the overall performance. Additionally, the nozzle had electromechanical actuators which replaced the heavier hydraulic ones used for thrust vector control. These developments could maybe have made their way back into

2805-448: Was on top of the main stage and below the payload. The original Ariane — Ariane 5G — used the EPS ( Étage à Propergols Stockables — Storable Propellant Stage), which was fueled by monomethylhydrazine (MMH) and nitrogen tetroxide , containing 10,000 kg (22,000 lb) of storable propellant . The EPS was subsequently improved for use on the Ariane 5G+, GS, and ES. The EPS upper stage

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2860-422: Was priced higher than the lower satellite, on the order of €90 million as of 2013 . Total launch price of an Ariane 5 – which could transport up to two satellites to space, one in the "upper" and one in the "lower" positions – was around €150 million as of January 2015 . The Ariane 5 ME (Mid-life Evolution) was in development into early 2015, and was seen as a stopgap between Ariane 5ECA/Ariane 5ES and

2915-498: Was reported early September instead of July. Nevertheless, SES-14 is still expected to be able to meet the designed lifetime. This satellite was originally to be launched with more propellant reserve on a Falcon 9 launch vehicle since the Falcon 9, in this specific case, was intended to deploy this satellite into a high inclination orbit that would require more work from the satellite to reach its final geostationary orbit. The Al Yah 3

2970-475: Was the heaviest single payload until the launch of the first ATV on 9 March 2008, at 19,360 kg (42,680 lb). The first launch of the ECA variant on 11 December 2002 ended in failure when a main booster problem caused the rocket to veer off-course, forcing its self-destruction three minutes into the flight. Its payload of two communications satellites ( STENTOR and Hot Bird 7 ), valued at about €630 million,

3025-557: Was the prime contractor for the manufacturing of the vehicles, leading a multi-country consortium of other European contractors. Ariane 5 was originally intended to launch the Hermes spacecraft, and thus it was rated for human space launches . Since its first launch, Ariane 5 was refined in successive versions: "G", "G+", "GS", "ECA", and finally, "ES". The system had a commonly used dual-launch capability, where up to two large geostationary belt communication satellites can be mounted using

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