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{{Infobox rocket
[[파일:MRO-launch.jpg|thumb|300px|아틀라스 5호의 발사장면]]
|image = MRO-launch.jpg
[[파일:MRO-launch.jpg|thumb|300px|caption = 아틀라스 5호의 발사장면]]
|제목 = Atlas V
|function = [[EELV]]/Medium-heavy [[launch vehicle]]
|manufacturer = [[United Launch Alliance]]
|country-origin = [[United States]]
|height = 58.3 m
|alt-height = 191.2 ft
|diameter = 3.81 m
|alt-diameter = 12.49 ft
|mass = 546,700 [[kilogram|kg]]
|alt-mass = 1,205,200 [[pound (mass)|lb]]
|stages = 2
|LEO-payload = 9,750 - 29,420 kg <ref name=product-sheet>{{cite web|format=PDF|제목=Atlas V Product Sheet|author=[[United Launch Alliance]]|url=http://www.ulalaunch.com/docs/product_sheet/AtlasProductSheetFINAL.pdf}}</ref>
|alt-LEO =
|payload-location = [[Geostationary transfer orbit|GTO]]
|payload = 4,950 - 13,000 kg <ref name=product-sheet/>
|alt-payload =
|status = Active
|sites = [[Cape Canaveral Air Force Station Launch Complex 41|LC-41]], [[Cape Canaveral Air Force Station|Cape Canaveral]]<br>[[Vandenberg AFB Space Launch Complex 3|SLC-3E]], [[Vandenberg Air Force Base|Vandenberg AFB]]
|launches = 15<br>('''401:''' 6, '''411:''' 2, '''421:''' 3, '''431:''' 1}<br>('''521:''' 2, '''551:''' 1)
|success = 14<br>('''401:''' 5, '''411:''' 2, '''421:''' 3, '''431:''' 1)<br>('''521:''' 2, '''551:''' 1)
|fail =
|partial = 1 ('''401''')<ref>[http://space.skyrocket.de/index_frame.htm?http://space.skyrocket.de/doc_lau_det/atlas-5-401.htm Gunter's Space Page - Atlas V (401)]</ref>
|first='''401:''' [[21 August]] [[2002]]<br>'''411:''' [[20 April]] [[2006]]<br>'''421:''' [[10 October]] [[2007]]<br>'''431:''' [[11 March]] [[2005]]<br>'''521:''' [[17 July]] [[2003]]<br>'''551:''' [[19 January]] [[2006]]
|last=
|payloads = [[Mars Reconnaissance Orbiter]]<br>[[New Horizons]]
|boosters = 1 to 5 (see text)
|diff = Not Heavy
|boostername = [[Aerojet]]
|boosterengines = 1 [[solid rocket|Solid]]
|boosterthrust = 1,270 [[newton|kN]]
|alt-boosterthrust = 285,500 [[pound-force|lb<sub>f</sub>]]
|boostertime = 94 seconds
|boosterSI = 275 sec
|boosterfuel = [[solid rocket|Solid]]
|alt-boosters = 2
|alt-diff = Atlas V Heavy (5HX)
|alt-boostername = Atlas [[Common Core Booster|CCB]]
|alt-boosterengines = 1 [[RD-180]]
|alt-boostersthrust = 4,152 [[newton|kN]]
|alt-alt-boosterthrust = 933,406 [[pound-force|lb<sub>f</sub>]]
|alt-boostertime = 253 seconds
|alt-boosterSI = 311 sec
|alt-boosterfuel = [[RP-1]]/[[LOX]]
|stage1name = Atlas [[Common Core Booster|CCB]]
|stage1engines = 1 [[RD-180]]
|stage1thrust = 4,152 [[newton|kN]]
|alt-stage1thrust = 933,406 [[pound-force|lb<sub>f</sub>]]
|stage1time = 253 seconds
|stage1SI = 311 sec
|stage1fuel = [[RP-1]]/[[LOX]]
|stage2name = [[Centaur (rocket stage)|Centaur]]
|stage2engines = 1 [[RL-10]]A
|stage2thrust = 99.2 kN
|alt-stage2thrust = 22,290 lb<sub>f</sub>
|stage2time = 842 seconds
|stage2SI = 451 sec
|stage2fuel = [[LH2]]/[[LOX]]
|stage2diff = Atlas V XX1
|stage2aname = [[Centaur (rocket stage)|Centaur]]
|stage2aengines = 2 [[RL-10]]A
|stage2athrust = 147 kN
|alt-stage2athrust = 41,592 lb<sub>f</sub>
|stage2atime = 421 seconds
|stage2aSI = 449 sec
|stage2afuel = [[LH2]]/[[LOX]]
|stage2adiff = Atlas V XX2
}}
 
'''아틀라스 5호'''(Atlas V)는 [[미국]]의 [[우주발사체]]이다. 러시아 엔진 [[RD-180]]을 사용하며, [[록히드 마틴]]이 [[미국 공군]]을 위해 개발했다. [[보잉]]이 개발한 [[델타 4호]] 로켓과 경쟁하고 있다. 2005년 부터 [[미국 공군]]의 우주 로켓인 [[타이탄 4호]]를 대체하여 [[케이프커내버럴 공군 기지]] 또는 [[반덴버그 공군 기지]]에서 발사되고 있다.
*[[H-IIB]]
*[[제니트]]
==참고==
 
{{주석}}
==같이 보기==
* [[반덴버그 공군 기지]]

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