Ariane 5: Perbedaan antara revisi
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Baris 1:
{{Infobox rocket
|name = Ariane 5
|image = Ariane 5ES with ATV 4 on its way to ELA-3.jpg
|caption = Ariane 5 ES yang mengangkut [[ATV-4]] didalamnya sedang menuju landasan peluncuran roket pada Juni 2013.
|function = Roket Kelas Berat
|manufacturer = [[Airbus Defence and Space]]<br/>Untuk [[European Space Agency|ESA]]
|country-origin = <!-- start collapsible list of ESA member states in attribute "country of origin" -->
{{Collapsible list
|titlestyle = background-color: #f9f9f9; text-align: left; font-weight: normal; line-height: 1.3em;
|liststyle = padding: 6px 0; background-color: none; text-align: left;
|framestyle = line-height: 2.0em; border: none; padding: 0;
|title = 20 ESA member states:
|[[Austria]]
|[[Belgium]]
|[[Czech Republic]]
|[[Denmark]]
|[[Finland]]
|[[France]]
|[[Germany]]
|[[Greece]]
|[[Ireland]]
|[[Italy]]
|[[Luxembourg]]
|[[Netherlands]]
|[[Norway]]
|[[Poland]]
|[[Portugal]]
|[[Romania]]
|[[Spain]]
|[[Sweden]]
|[[Switzerland]]
|[[United Kingdom]]
}}
| cpl = €139–185 million <ref name=capabilities>{{cite web|title=Arianespace aims high in Asia-Pacific|url=https://www.flightglobal.com/news/articles/arianespace-aims-high-in-asia-pacific-425928/
|publisher=Flightglobal|access-date=1 June 2016|archive-url=https://web.archive.org/web/20160602105116/https://www.flightglobal.com/news/articles/arianespace-aims-high-in-asia-pacific-425928/|archive-date=2 June 2016|url-status=live}}</ref>
|height = {{cvt|46|-|52|m}}
|diameter = {{cvt|5.4|m}}
|mass = {{cvt|777000|kg}}
|stages = 2
|capacities =
{{Infobox rocket/payload
|location = [[Low Earth orbit]]
|altitude = {{cvt|260|km}} (circular)
|inclination = 51.6°
|kilos = '''G:''' {{cvt|16000|kg}}<br/>'''ES:''' over {{cvt|20000|kg}}<ref name=ESAA5ES/>
}}
{{Infobox rocket/payload
|location = [[Geostationary transfer orbit|GTO]]
|kilos = {{plainlist|
* '''G:''' {{cvt|6950|kg}}
* '''G+:''' {{cvt|6950|kg}}
* '''GS:''' {{cvt|6100|kg}}
* '''ECA:''' {{cvt|10865|kg}}<ref name=final-10>{{cite web|url=http://www.spacedaily.com/reports/Arianespace_begins_building_final_10_Ariane_5s_ahead_of_Ariane_6_operational_debut_999.html|title=Arianespace begins building final 10 Ariane 5s ahead of Ariane 6 operational debut|website=Space Daily|access-date=10 January 2019|archive-url=https://web.archive.org/web/20190201014945/http://www.spacedaily.com/reports/Arianespace_begins_building_final_10_Ariane_5s_ahead_of_Ariane_6_operational_debut_999.html|archive-date=1 February 2019|url-status=live}}</ref>
}}
}}
| family = [[Ariane (rocket family)|Ariane]]
| comparable = {{plainlist|
* [[Atlas V|Atlas V 551]]
* [[Delta IV Heavy]]
* [[Falcon 9 Block 5]]
* [[H-IIB]]
* [[Long March 5]]
* [[Proton-M]]
}}
|status = {{plainlist|
* '''G:''' Retired
* '''G+:''' Retired
* '''GS:''' Retired
* '''ECA:''' Active
* '''ES:''' Retired
}}
|sites = [[Guiana Space Centre|Centre Spatial Guyanais]], [[ELA-3]]
|launches = 110 {{hlist| '''G:''' 16 | '''G+:''' 3 | '''GS:''' 6 }} {{hlist| '''ECA:''' 77 | '''ES:''' 8 }} <!-- UPDATE after each flight -->
|success = 105 {{hlist| '''G:''' 13 | '''G+:''' 3 | '''GS:''' 6 }} {{hlist| '''ECA:''' 76 | '''ES:''' 8 }}
|fail = 2 ('''G:''' 1, '''ECA:''' 1)
|partial = 3 ('''G:''' 2, '''ECA:''' 1)
|first = {{plainlist|
* '''G:''' 4 June 1996
* '''G+:''' 2 March 2004
* '''GS:''' 11 August 2005
* '''ECA:''' 11 December 2002
* '''ES:''' 9 March 2008
}}
|last = {{plainlist|
* '''G:''' 27 September 2003
* '''G+:''' 18 December 2004
* '''GS:''' 18 December 2009
* '''ECA:''' 30 July 2021
* '''ES:''' 25 July 2018
}}
|payloads = {{plainlist|
* [[XMM-Newton]]
* [[Envisat]]
* [[Rosetta (spacecraft)|Rosetta]]
* [[Automated Transfer Vehicle|ATV]]
* [[Herschel Space Observatory|Herschel]]
* [[Planck (spacecraft)|Planck]]
* [[Galileo (satellite navigation)|Galileo]]
}}
|stagedata =
{{Infobox rocket/stage
|type = booster
|diff = G, G+
|stageno = zero
|name = EAP P238
|number = 2
|length = {{cvt|31.6|m}}
|diameter = {{cvt|3.06|m}}
|empty =
|gross = {{cvt|270|MT}}
|engines = P238
|thrust = {{cvt|6650|kN}}
|total = {{cvt|13300|kN}}
|SI = <!-- specific impulse of an individual booster, in secs, optional -->
|burntime = 130 seconds
|fuel = [[Ammonium perchlorate|AP]], [[Aluminium]], [[Hydroxyl-terminated polybutadiene|HTPB]]
}}
{{Infobox rocket/stage
|type = booster
|diff = GS, ECA, ES
|stageno = zero
|name = EAP P241
|number = 2
|length = {{cvt|31.6|m}}
|diameter = {{cvt|3.06|m}}
|empty = {{cvt|33|MT}}
|gross = {{cvt|273|MT}}
|engines = P241
|thrust = {{cvt|7080|kN}}
|total = {{cvt|14160|kN}}
|SI = <!-- specific impulse of an individual booster, in secs, optional -->
|burntime = 140 seconds
|fuel = [[Ammonium perchlorate|AP]], [[Aluminium]], [[Hydroxyl-terminated polybutadiene|HTPB]]
}}
{{Infobox rocket/stage
|type = stage
|diff = G, G+, GS
|stageno = Core
|name = EPC H158
|length = {{cvt|23.8|m}}
|diameter = {{cvt|5.4|m}}
|empty = {{cvt|12200|kg}}
|gross = {{cvt|170500|kg}}
|engines = G, G+: [[Vulcain (rocket engine)|Vulcain]] 1 <br/> GS: [[Vulcain (rocket engine)|Vulcain]] 1B
|thrust = {{cvt|1015|kN}} (vacuum)
|SI = 440 seconds (vacuum)
|burntime = 605 seconds
|fuel = [[LH2|LH<sub>2</sub>]] / [[LOX]]
}}
{{Infobox rocket/stage
|type = stage
|diff = ECA, ES
|stageno = Core
|name = EPC H173
|length = {{cvt|23.8|m}}
|diameter = {{cvt|5.4|m}}
|empty = {{cvt|14700|kg}}
|gross = {{cvt|184700|kg}}
|engines = [[Vulcain (rocket engine)|Vulcain]] 2
|thrust = {{cvt|960|kN}}<br/>(sea level)<br/>{{cvt|1390|kN}} (vacuum)
|SI = 310 seconds (sea level)<br/>432 seconds (vacuum)
|burntime = 540 seconds
|fuel = [[LH2|LH<sub>2</sub>]] / [[LOX]]
}}
{{Infobox rocket/stage
|type = stage
|diff = G
|stageno = Second
|name = EPS L9.7
|length = {{cvt|3.4|m}}
|diameter = {{cvt|5.4|m}}
|empty = {{cvt|1200|kg}}
|gross = {{cvt|10900|kg}}
|engines = [[Aestus]]
|thrust = {{cvt|27|kN}}
|SI = <!-- specific impulse of an individual stage, in secs, optional -->
|burntime = 1100 seconds
|fuel = [[Monomethylhydrazine|MMH]] / [[Nitrogen tetroxide|N<sub>2</sub>O<sub>4</sub>]]
}}
{{Infobox rocket/stage
|type = stage
|diff = G+, GS, ES
|stageno = Second
|name = EPS L10
|length = {{cvt|3.4|m}}
|diameter = {{cvt|5.4|m}}
|empty = {{cvt|1200|kg}}
|gross = {{cvt|11200|kg}}
|engines = [[Aestus]]
|thrust = {{cvt|27|kN}}
|SI = <!-- specific impulse of an individual stage, in secs, optional -->
|burntime = 1170 seconds
|fuel = [[Monomethylhydrazine|MMH]] / [[Nitrogen tetroxide|N<sub>2</sub>O<sub>4</sub>]]
}}
{{Infobox rocket/stage
|type = stage
|diff = ECA
|stageno = Second
|name = ESC-A
|length = {{cvt|4.711|m}}
|diameter = {{cvt|5.4|m}}
|empty = {{cvt|4540|kg}}
|gross = {{cvt|19440|kg}}
|engines = [[HM7B]]
|thrust = {{cvt|67|kN}}
|SI = 446 seconds
|burntime = 945 seconds
|fuel = [[LH2|LH<sub>2</sub>]] / [[LOX]]
}}
}}
'''Ariane 5''' adalah sebuah [[sistem peluncuran sekali pakai]] (''expendable launch system'') yang dirancang untuk mengantarkan [[satelit]] ke [[orbit transfer geostationer]] dan untuk mengirim muatan ke [[orbit bumi rendah]].
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