Editing Ariane 4

{{Short description|Rocket}}
{{Use British English|date=January 2014}}
{{Use dmy dates|date=May 2020}}
{{Infobox rocket
| name          = Ariane 4
| image         = Ariane42P rocket.png
| caption       = The 52nd Ariane 4 carrying the [[TOPEX/Poseidon]] satellite.
| upright       = 1.3

|function       = Expendable [[launch vehicle]]
|manufacturer   = [[Aérospatiale]]
|country-origin = [[Europe]]
|height         = {{cvt|58.72|m}}
|diameter       = {{cvt|3.8|m}}
|mass           = {{cvt|240,000|–|470,000|kg}}

|stages         = 3<ref>{{Cite web |editor-last=Wade |editor-first=Mark |title=Ariane 4 |url=http://www.astronautix.com/a/ariane4.html |url-status=live |archive-url=https://web.archive.org/web/20161228030559/http://astronautix.com/a/ariane4.html |archive-date=28 December 2016 |access-date=22 June 2021 |website=Encyclopedia Astronautica }}</ref>
|capacities =
  {{Infobox Rocket/Payload
  |location     = [[Low Earth orbit|LEO]]{{No orbit for payload inline|date=September 2020}}
  |kilos        = {{cvt|5000|–|7600|kg}}
  }}
  {{Infobox Rocket/Payload
  |location     = [[Geosynchronous transfer orbit|GTO]]
  |kilos        = {{cvt|2000|–|4300|kg}}
  }}
|status         = Retired
|sites          = [[Kourou]], [[ELA-2]]
|launches       = 116<br/>('''40:''' 7, '''42P:''' 15, '''42L:''' 13)<br/>('''44P:''' 15, '''44LP:''' 26, '''44L:''' 40)
|success        = 113<br/>('''40:''' 7, '''42P:''' 14, '''42L:''' 13)<br/>('''44P:''' 15, '''44LP:''' 25, '''44L:''' 39)
|fail           = 3 ('''42P:''' 1, '''44L:''' 1, '''44LP:''' 1)
|first={{ubl
 | '''40:''' 22 January 1990
 | '''42P:''' 20 November 1990
 | '''42L:''' 12 May 1993
 | '''44P:''' 4 April 1991
 | '''44LP:''' 15 June 1988
 | '''44L:''' 5 June 1989
 }}
|last={{ubl
 | '''40:''' 3 December 1999
 | '''42P:''' 4 May 2002
 | '''42L:''' 23 January 2002
 | '''44P:''' 25 September 2001
 | '''44LP:''' 27 November 2001
 | '''44L:''' 15 February 2003
 }}
|stagedata     =
  {{Infobox Rocket/Stage
  |type        = booster
  |diff        = Ariane 42L, 44LP or 44L
  |stageno     = Booster
  |name        = PAL
  |number      = 0, 2 or 4
  |engines     = [[Viking (rocket engine)|Viking 6]]
  |thrust      = {{cvt|752.003|kN|lbf}}
  |total       = <!--total thrust for all boosters in kN, optional-->
  |alt-total   = <!--total thrust for all boosters in pounds-force, optional-->
  |SI          = 278 seconds
  |burntime    = 142 seconds
  |fuel        = [[Dinitrogen tetroxide|N<sub>2</sub>O<sub>4</sub>]] / [[UDMH]]
  }}
  {{Infobox Rocket/Stage
  |type        = booster
  |diff        = Ariane 42P, 44LP or 44P
  |stageno     = Booster
  |name        = PAP
  |number      = 0, 2 or 4
  |engines     = <!--number and type of engines used on each individual booster/stage, required-->
  |thrust      = {{cvt|650|kN|lbf}}
  |total       = <!--total thrust for all boosters in kN, optional-->
  |SI          = <!--specific impulse of an individual booster/stage, in secs, optional-->
  |burntime    = 33 seconds
  |fuel        = CTPB 1613
  }}
  {{Infobox Rocket/Stage
  |type        = stage
  |stageno     = First
  |name        = L220
  |engines     = 4 [[Viking (rocket engine)|Viking 5C]]
  |thrust      = {{cvt|3,034.1|kN|lbf}}
  |total       = <!--total thrust for all boosters in kN, optional-->
  |SI          = 278 seconds
  |burntime    = 205 seconds
  |fuel        = [[Dinitrogen tetroxide|N<sub>2</sub>O<sub>4</sub>]] / [[UDMH]]
  }}
  {{Infobox Rocket/Stage
  |type        = stage
  |stageno     = Second
  |name        = L33
  |engines     = 1 [[Viking (rocket engine)|Viking 4B]]
  |thrust      = {{cvt|720.965|kN|lbf}}
  |total       = <!--total thrust for all boosters in kN, optional-->
  |SI          = 296 seconds
  |burntime    = 132 seconds
  |fuel        = [[Dinitrogen tetroxide|N<sub>2</sub>O<sub>4</sub>]] / [[UDMH]]
  }}
  {{Infobox Rocket/Stage
  |type        = stage
  |diff        = <!--variant of rocket this is used on, optional-->
  |stageno     = Third
  |name        = H10
  |engines     = 1 [[HM7-B]]
  |thrust      = {{cvt|62.703|kN|lbf}}
  |total       = <!--total thrust for all boosters in kN, optional-->
  |SI          = 446 seconds
  |burntime    = 759 seconds
  |fuel        = [[LH2|LH{{sub|2}}]] / [[LOX]]
  }}
}}

The '''Ariane 4''' was a European [[expendable rocket|expendable]] [[launch vehicle]], developed by the {{lang|fr|[[CNES|Centre national d'études spatiales]]}} (CNES), the [[Government of France|French]] space agency, for the [[European Space Agency]] (ESA). The manufacturing of the launch vehicle was led by [[Aérospatiale]] and it was marketed by [[Arianespace]]. Since its first flight on 15 June 1988 until the final flight on 15 February 2003, it attained 113 successful launches out of 116 total launches.

In 1982, the Ariane 4 program was approved by ESA. Drawing heavily upon the preceding [[Ariane 3]], it was designed to provide a launcher capable of delivering heavier payloads and at a lower cost per kilogram than the earlier members of the Ariane family. The Ariane 4 was principally an evolution of the existing technologies used, as opposed to being revolutionary in its design ethos; this approach quickly gained the backing of most ESA members, who funded and participated in its development and operation. Capable of being equipped with a wide variety of [[Booster (rocketry)|strap-on booster]]s, the Ariane 4 gained a reputation for being an extremely versatile launcher.

Once in service, the launcher soon became recognized for being ideal for launching communications and [[Earth observation satellite]]s, as well as those used for scientific research. During its working life, the Ariane 4 managed to capture 50% of the market in launching commercial satellites, soundly demonstrating Europe's ability to compete in the commercial launch sector.<ref name="esa-ariane4">{{Cite web |date=14 May 2004 |title=Ariane 4 |url=https://www.esa.int/Enabling_Support/Space_Transportation/Ariane_42 |url-status=live |archive-url=https://web.archive.org/web/20231203233822/https://www.esa.int/Enabling_Support/Space_Transportation/Ariane_42 |archive-date=3 December 2023 |access-date=13 June 2015 |publisher=[[European Space Agency]] }}</ref> In February 2003, the final Ariane 4 was launched; Arianespace had decided to retire the type in favour of the newer and larger [[Ariane 5]], which effectively replaced it in service.

== Development ==
=== Origins ===
In 1973, eleven nations decided to pursue joint collaboration in the field of space exploration and formed a new pan-national organisation to undertake this mission, the [[European Space Agency]] (ESA).<ref name="harvey-2003">{{cite book |first=Brian |last=Harvey |title=Europe's Space Programme: To Ariane and Beyond |year=2003 |publisher=Springer Science & Business Media |isbn=1-8523-3722-2 }}</ref>{{rp|pages=161-162}} Six years later, in December 1979, the arrival of a capable European [[expendable launch system]] was marked when the first [[Ariane 1]] launcher was successfully launched from the [[Guiana Space Centre|Centre Spatial Guyanais]] (CSG) at [[Kourou]], [[French Guiana]].<ref name="harvey-2003" />{{rp|page=169}} The Ariane 1 soon became considered to be a capable and competitive launcher in comparison to rival platforms offered by the [[Soviet Union]] and the [[United States|United States of America]], and it was quickly followed by improved derivatives in the form of the [[Ariane 2]] and [[Ariane 3]]. By early 1986, the Ariane 1, along with the Ariane 2 and Ariane 3, had become the dominant launcher on the world market.<ref name="harvey-2003" />{{rp|page=172}}

In January 1982, the ESA issued its authorisation for the development and construction of the Ariane 4; the development programme had the stated objective of increasing the usable payload by 90%.<ref name= "encyc aria"/> The Ariane 4 would be a considerably larger and more flexible launcher that the earlier members of its family, being intended to compete with the upper end of launchers worldwide. In comparison, while the Ariane 1 had a typical weight of {{convert|207|t|lb}} and could launch payloads of up to {{convert|1.7|t|lb}} into orbit; the larger Ariane 4 had a typical weight of {{convert|470|t|lb}} and could orbit payloads of up to {{convert|4.2|t|lb}}.<ref name="harvey-2003" />{{rp|page=178}} Work on the Ariane 4 was substantially eased via drawing heavily on both the technology and experiences gained from producing and operating the earlier members of the [[Ariane (rocket family)|Ariane rocket]]. The total development cost for the Ariane 4 was valued at 476 million [[European Currency Unit]]s (ECU) in 1986.<ref name="encyc aria">{{Cite web |editor-last=Wade |editor-first=Mark |title=Ariane |url=http://www.astronautix.com/a/ariane.html |url-status=live |archive-url=https://web.archive.org/web/20240207065823/http://www.astronautix.com/a/ariane.html |archive-date=7 February 2024 |access-date=13 June 2015 |website=Encyclopedia Astronautica }}</ref>

Posed with the requirement to produce a rocket with substantially greater thrust, the design team considered various approaches to achieve this.<ref name="harvey-2003" />{{rp|page=179}} One concept studied had involved the addition of a fifth engine to an enlarged first stage of the Ariane 3, but was found to involve a very high level of redesign work to achieve this; instead, the first stage was elongated to hold {{convert|210|t|lb}} of propellant instead of the {{convert|145|t|lb}} present on the Ariane 3. While the second and third stages remained identical to the Ariane 3, a range of [[Booster (rocketry)|strap-on booster]]s were developed to be applied to the type, designed to gradually increase the rocket's payload capacity.<ref name="harvey-2003" />{{rp|page=179}} Overall, the Ariane 4 was 15% smaller than the Ariane 3.<ref name="harvey-2003" />{{rp|page=180}}

In effect, the Ariane 4 was an improved and developed derivative of the earlier Ariane 3, primarily differing through the application of various [[Solid rocket booster|solid]]-fuelled and [[liquid rocket booster|liquid]]-fuelled boosters, the latter being the only all-new design feature of the Ariane 4; at this point, the practice of using liquid boosters was uncommon, having only previously been used in the [[Chinese space program]].<ref name="harvey-2003" />{{rp|page=179}} Another innovation of the Ariane 4 was the dual-launch SPELDA (Structure Porteuse Externe de Lancement Double Ariane) fairing.<ref name="harvey-2003" />{{rp|page=180}} This had the function of allowing a pair of satellites, one placed on top of the other; several different SPELDA nose fairings could be installed, including normal and extended models. The SPELDA was considerably lighter than its predecessor; the guidance system also used much more accurate [[ring laser gyroscope]]s.<ref name="harvey-2003" />{{rp|page=180}} According to aviation author Brian Harvey, the advances present in the design of the Ariane 4 represented a conservative and evolutionary, rather than revolutionary, philosophy.<ref name="harvey-2003" />{{rp|page=180}}

=== Teaming and construction ===
As the Ariane 4 programme took shape, it gained the support of [[Belgium]], [[Denmark]], [[Spain]], [[Ireland]], [[Italy]], the [[Netherlands]], [[Germany]], the [[United Kingdom]], [[France]], [[Sweden]], and [[Switzerland]].<ref name="harvey-2003" />{{rp|page=180}} The main contractors were [[Aérospatiale]] (responsible for the first and second stages), [[Messerschmitt-Bölkow-Blohm]] (MBB) (produced the liquid-fuelled boosters), [[Safran Aircraft Engines|Société Européenne de Propulsion]] (SEP) (engine manufacturer), [[Matra]] (equipment bay assembly), [[Air Liquide]] (production of third stage tanks and insulation), [[SNIA S.p.A.|BPD Snia]] (maker of solid-fuelled boosters), and [[British Aerospace]]/[[RUAG|Contraves Space AG]] (manufacturers of the fairing).<ref name="harvey-2003" />{{rp|page=180}} For their work on the Ariane 4, the Launch Team were subsequently awarded the Space Achievement Award by the [[Space Foundation]] in 2004.<ref>{{Cite web |title=Awards |url=https://www.spacefoundation.org/what-we-do/awards/ |url-status=live |archive-url=https://web.archive.org/web/20240519040331/https://www.spacefoundation.org/what-we-do/awards/ |archive-date=19 May 2024 |access-date=13 June 2015 |publisher=[[Space Foundation]] }}</ref>

In conjunction with the development of the Ariane 4 itself, a new purpose-built launch preparation area and launch pad for the rocket, collectively designated as ''ELA-2'', was constructed at the [[Guiana Space Centre|Centre Spatial Guyanais]] to service the Ariane 4 and provide a launch rate of 8 launches per year (this feat was near-unprecedented for a single large rocket, other than within the Soviet Union).<ref name="harvey-2003" />{{rp|pages=178-179}} Unlike the earlier ''ELA-1'' which had been used for the previous members of the Ariane family and other rockets, preparation activity for the rocket would be performed in a purpose-built {{convert|80|m|ft|adj=on}} tall hall rather than on the pad itself; the completed rocket was then transported using a specially-designed railway to slowly traverse from the hall to the launch pad, taking one hour. This railway provided the additional benefit of enabling faulty rockets to be withdrawn from the pad and be substituted for relatively quickly.<ref name="harvey-2003" />{{rp|page=179}}

On 15 June 1988, the first successful launch of the Ariane 4 was conducted.<ref name="harvey-2003" />{{rp|page=180}} For this first test flight, it was decided to fire the second most powerful version of the rocket, designated ''44LP'', equipped with four main engines, two solid boosters and two liquid boosters; it was also furnished with the multi-satellite SPELDA fairing. 50 seconds after take-off, the solid boosters would be expended and be detached in order to reduce the rocket's weight.<ref name="harvey-2003" />{{rp|page=180}} 143 seconds after take-off, the liquid boosters also detached, further lightening the vehicle. The maiden flight was considered a success, putting multiple satellites into orbit.<ref name="harvey-2003" />{{rp|page=180}}

=== Further development ===
For the V50 launch onwards, an improved third stage, known as the ''H10+'', was adopted for the Ariane 4.<ref name="harvey-2003" />{{rp|page=183}} The H10+ third stage featured a new tank, which was {{cvt|26|kg|lb}} lighter, {{cvt|32|cm|in}} longer, and contained {{cvt|340|kg|lb}} more fuel, which raised the rocket's overall payload capacity by {{cvt|110|kg|lb}} and increased its burn time by 20&nbsp;seconds.<ref name="harvey-2003" />{{rp|page=183}}

Even prior to the first flight of the Ariane 4, development of a successor, designated as the [[Ariane 5]], had already commenced.<ref name="harvey-2003" />{{rp|pages=184-185}} In January 1985, the Ariane 5 had been officially adopted as an ESA programme. It lacked the high levels of commonality that the Ariane 4 had with its predecessors, and had been designed not only for launching heavier payloads of up to {{convert|5.2|t|lb}} and at a 20% cost reduction over the Ariane 4, but for a higher margin of safety due to the fact that the Ariane 5 was designed to conduct crewed space launches as well, being intended to transport [[astronaut]]s using the proposed [[Hermes (spacecraft)|Hermes space vehicle]].<ref name="harvey-2003" />{{rp|page=185}} Development of the Ariane 5 was not without controversy as some ESA members considered the more mature Ariane 4 to be more suited for meeting established needs for such launchers; it was for this reason that Britain chose not to participate in the Ariane 5 programme.<ref name="harvey-2003" />{{rp|page=186}} For some years, Ariane 4 and Ariane 5 launchers were operated interchangeably; however, it was eventually decided to terminate all Ariane 4 operations in favour of concentrating on the newer Ariane 5.<ref name="harvey-2003" />{{rp|page=193}}

== Design ==
The Ariane 4 was the ultimate development from the preceding members of the [[Ariane (rocket family)|Ariane rocket family]]. Compared with the [[Ariane 2]] and [[Ariane 3]], the Ariane 4 featured a stretched first (by 61%) and third stages, a strengthened structure, new propulsion bay layouts, new avionics, and the SPELDA (''Structure Porteuse Externe de Lancement Double Ariane'') dual-payload carrier. The basic 40 version did not employ any strap-on motors, while the Ariane 42L, 44L, 42P, 44P, and 44LP variants all used various combinations of [[solid rocket booster|solid]] and [[Liquid rocket booster|liquid]] [[strap-on booster|boosters]]. Originally designed to place {{cvt|2000|to|4200|kg|lb}} payloads in [[geostationary orbit]], the six Ariane 4 variants, aided by strap-on boosters, enabled the launch of payloads in excess of {{cvt|4900|kg|lb}} on several occasions. The Ariane 4 launcher reduced the launch costs per kilo by 55% in comparison to the original [[Ariane 1]].<ref name="harvey-2003" />{{rp|page=180}}

The rocket was used in a number of variants - it could be fitted with two or four additional [[solid rocket booster|solid]] (PAP for ''Propulseurs d'Appoint à Poudre'') or [[Liquid rocket booster|liquid]] fueled booster rockets (PAL for ''Propulseurs d'Appoint à Liquide''). The launcher included a satellite payload carrier system called ''SPELDA'' (''Structure porteuse externe de lancement double Ariane'', French for ''External Carrying Structure for Ariane Double Launches'') for launching more than one satellite at a time. The rocket captured nearly 60% of the world's commercial launch services market, serving both European and international clients.<ref>{{Cite web |date=9 June 2015 |title=Ariane 4, un défi pour l'Europe spatiale |trans-title=Ariane 4 - A challenge for Europe's space industry |url=https://ariane.cnes.fr/fr/web/CNES-fr/308-ariane-4-un-defi.php |url-status=live |archive-url=https://web.archive.org/web/20230923063802/https://ariane.cnes.fr/fr/web/CNES-fr/308-ariane-4-un-defi.php |archive-date=23 September 2023 |access-date=13 June 2015 |publisher=[[CNES]] |language=fr }}</ref> Atop the third stage was a vehicle equipment stage which housed a computer that performed various functions, including sequencing, guidance, control, tracking, [[telemetry]] and an explosive-based self-destruct.<ref name="harvey-2003" />{{rp|page=180}}

The Ariane 4 AR 40 was the basic version, with three stages: {{cvt|58.4|m|ft}} high, a diameter of {{cvt|3.8|m|ft}}, a liftoff mass of {{cvt|245000|kg|lb}} and a maximum payload of {{cvt|2100|kg|lb}} to GTO or {{cvt|5000|kg|lb}} to [[low Earth orbit]] (LEO). Main power was provided by four [[Viking (rocket engine)|Viking 2B motors]], each producing {{cvt|667|kN|lbf}} of thrust. The second stage was powered by a single Viking 4B motor, and the third stage was equipped with an [[HM7-B]] liquid oxygen/liquid hydrogen motor. The Ariane 4 AR 44L, which was outfitted with the maximum additional boost of four liquid fuel rocket strap-ons, was a four-stage rocket, weighing {{cvt|470000|kg|lb}} and capable of transferring a payload of {{cvt|4730|kg|lb}} to GTO, or alternatively {{cvt|7600|kg|lb}} to LEO.

[[File:Ariane4.gif|thumb|upright=2.0|center|5 of the 6 versions of Ariane 4]]

{| class="wikitable" style="margin:1em auto 1em auto; text-align:center;"
! Model
! PAL
! PAP
! Payload to [[Geostationary transfer orbit|GTO]] (kg)
! Launches
! Successes
! Failure date
|-----
| style="text-align:left;" | AR 40
| 0 || 0 || 2100 || 7 || 7
| 
|-----
| style="text-align:left;" | AR 42P
| 0 || 2 || 2930 || 15 || 14
| 1 December 1994
|-----
| style="text-align:left;" | AR 42L
| 2 || 0 || 3480 || 13 || 13
| 
|-----
| style="text-align:left;" | AR 44P
| 0 || 4 || 3460 || 15 || 15
| 
|-----
| style="text-align:left;" | AR 44LP
| 2 || 2 || 4220 || 26 || 25
| 24 January 1994
|-----
| style="text-align:left;" | AR 44L
| 4 || 0 || 4720 || 40 || 39
| 22 February 1990
|}

== Operational history ==
{{main|List of Ariane launches}}

In June 1988, the inaugural flight of the Ariane 4 occurred, which was a success. Since then, Ariane 4 has flown 116 times, 113 of which were successful, yielding a success rate of {{percent|113|116|1}}. 

On 22 February 1990, the first failure occurred during the eighth Ariane 4 launch, flight V36. The rocket exploded 9 km above Kourou.<ref name="harvey-2003" />{{rp|pages=182-183}} The failure occurred because a worker assembling a [[Viking (rocket engine)|Viking rocket motor]] had left a handkerchief in one of the motor's coolant tubes. He had done so as a reminder to himself to inform his superior, as per procedure, of an unplanned polishing he had made to fit the tube. But he fell ill before he could do so and was replaced by other workers who did not notice the handkerchief. In flight, the handkerchief blocked the coolant tube, the motor overheated and failed, and the Ariane self-destructed after veering off its trajectory. Its payload, two communications satellites worth 500 million US dollars ([[Superbird-B]] and [[BS-2X]]) landed in pieces in the swamps near Kourou.<ref name=":0">{{Cite web |last=Castanos |first=Francis |date=7 December 2020 |title=The Space Review: The cloth of doom: The weird, doomed ride of Ariane Flight 36 |url=https://www.thespacereview.com/article/4085/1 |url-status=live |archive-url=https://web.archive.org/web/20231204195450/https://thespacereview.com/article/4085/1 |archive-date=4 December 2023 |access-date=25 December 2021 |website=www.thespacereview.com }}</ref> The ensuing investigation recommended 44 modifications, including numbering and checking all pieces of cloth used in the rocket's assembly.<ref name=":0" /> The following 26 launches were all completed successfully.<ref name="harvey-2003" />{{rp|page=183}}

The system became the basis for European [[satellite]] launches with a record of 113 successful and three launch failures. Ariane 4 provided a payload increase from {{cvt|1700|kg|lb}} for [[Ariane 3]] to a maximum of {{cvt|4800|kg|lb}} to [[geostationary transfer orbit]] (GTO). The record for Ariane 4 to GTO was {{cvt|4946|kg|lb}}.<ref>{{cite web|url=http://www.space-airbusds.com/en/programmes/ariane-4.html|title=Ariane 4|publisher=Airbus Defence and Space|access-date=13 June 2015|archive-date=27 September 2016|archive-url=https://web.archive.org/web/20160927235322/http://www.space-airbusds.com/en/programmes/ariane-4.html|url-status=dead}}</ref>

On 15 February 2003, the final launch of Ariane 4 rocket occurred, placing [[Intelsat 907]] into [[geosynchronous orbit]].<ref name="arianespace-20030215">{{Cite press release |date=15 February 2003 |title=Arianespace Flight 159: Mission Accomplished! 23rd launch for Intelsat |url=https://www.arianespace.com/press-release/arianespace-flight-159-mission-accomplished-23rd-launch-for-intelsat/ |url-status=live |archive-url=https://web.archive.org/web/20230706025156/https://www.arianespace.com/press-release/arianespace-flight-159-mission-accomplished-23rd-launch-for-intelsat/ |archive-date=6 July 2023 |access-date=28 May 2024 |publisher=[[Arianespace]] }}</ref> Arianespace had decided to phase out the Ariane 4 launcher in favour of the newer heavy-lift [[Ariane 5]] rocket, which had already been in service for some years. In 2011, the medium-lift [[Soyuz-2|Soyuz ST]] complemented the offering of launch vehicles from the [[Soyuz at the Guiana Space Centre|Centre Spatial Guyanais]]. Spacecraft launched by the Soyuz reused the payload platform and dispenser which had been originally designed for the Ariane.<ref>{{Cite web |date=March 2012 |title=Soyuz User's Manual |url=http://www.arianespace.com/launch-services-soyuz/Soyuz-Users-Manual-March-2012.pdf |url-status=dead |archive-url=https://web.archive.org/web/20131228235729/http://www.arianespace.com/launch-services-soyuz/Soyuz-Users-Manual-March-2012.pdf |archive-date=28 December 2013 |access-date=13 June 2015 |publisher=[[Arianespace]] }}</ref>

== Comparable rockets ==
* [[Delta II]] (retired)
* [[GSLV|GSLV Mk II]]
* [[GSLV Mk III]]
* [[Long March 3B]]
* [[Soyuz-U]] (retired)

== See also ==
{{Portal|Spaceflight}}
* [[Comparison of orbital launchers families]]
* [[Tsyklon-4]] (Ukrainian carrier rocket with fairing derived from Ariane 4)

== References ==
{{Reflist|30em}}

== External links ==
{{Commons category|Ariane 4}}
* [http://www.esa.int/Our_Activities/Launchers/Ariane_42 ESA Ariane 4 launchers]
* [https://fas.org/spp/guide/europe/launch/ariane4.htm FAS Ariane 4] {{Webarchive|url=https://web.archive.org/web/20160314015540/https://fas.org/spp/guide/europe/launch/ariane4.htm |date=14 March 2016 }}
* [https://www.flickr.com/photos/27417638@N07/7411229284/in/photolist- A cutaway drawing of the Ariane 4]

{{Ariane}}
{{Expendable launch systems}}
{{European launch systems}}

[[Category:Ariane (rocket family)]]
[[Category:Vehicles introduced in 1988]]