Atlas V


Atlas V is the fifth major version in the Atlas rocket family. It is an expendable launch system originally designed by Lockheed Martin, now being operated by United Launch Alliance, a joint venture between Lockheed and Boeing.
Each Atlas V rocket consists of two main stages. The first stage is powered by a Russian RD-180 engine manufactured by RD Amross and burning kerosene and liquid oxygen. The Centaur upper stage is powered by one or two US RL10 engine manufactured by Aerojet Rocketdyne and burning liquid hydrogen and liquid oxygen. AJ-60A strap-on solid rocket boosters are used in some configurations and will be replaced by GEM-63 SRBs in the near future. The standard payload fairings are 4 or 5 meters in diameter with various lengths.

Vehicle description

The Atlas V was developed by Lockheed Martin Commercial Launch Services as part of the US Air Force Evolved Expendable Launch Vehicle program and made its inaugural flight on August 21, 2002. The vehicle operates from Space Launch Complex 41 at Cape Canaveral Air Force Station and Space Launch Complex 3-E at Vandenberg Air Force Base. LMCLS continued to market the Atlas V to commercial customers worldwide until January 2018, when ULA assumed control of commercial marketing and sales.

Atlas V first stage

The Atlas V first stage, the Common Core Booster, is 12.5 ft in diameter and 106.6 ft in length. It is powered by one Russian RD-180 main engine burning 627,105 lb of liquid oxygen and RP-1. The booster operates for about four minutes, providing about 4 meganewtons of thrust. Thrust can be augmented with up to five Aerojet strap-on solid rocket boosters, each providing an additional 1.27 meganewtons of thrust for 94 seconds.
The Atlas V is the newest member of the Atlas family. Compared to the Atlas III vehicle, there are numerous changes. Compared to the Atlas II, the first stage is a near-redesign. There was no Atlas IV.
The main differences between the Atlas V and earlier Atlas I and II family rockets are:
The Centaur upper stage uses a pressure-stabilized propellant-tank design and cryogenic propellants. The Centaur stage for Atlas V is stretched 5.5 ft relative to the Atlas IIAS Centaur and is powered by either one or two Aerojet Rocketdyne RL10A-4-2 engines, each engine developing a thrust of 99.2 kN. The inertial navigation unit located on the Centaur provides guidance and navigation for both the Atlas and Centaur and controls both Atlas and Centaur tank pressures and propellant use. The Centaur engines are capable of multiple in-space starts, making possible insertion into low Earth parking orbit, followed by a coast period and then insertion into GTO. A subsequent third burn following a multi-hour coast can permit direct injection of payloads into geostationary orbit., the Centaur vehicle had the highest proportion of burnable propellant relative to total mass of any modern hydrogen upper stage and hence can deliver substantial payloads to a high-energy state.

Payload fairing

Atlas V payload fairings are available in two diameters, depending on satellite requirements. The 4.2 meter diameter fairing, originally designed for the Atlas II booster, comes in three different lengths: the original 9-meter-long version and extended 10-meter and 11-meter versions, first flown respectively on the AV-008/Astra 1KR and AV-004/Inmarsat-4 F1 missions. Fairings of up to 7.2 m diameter and 32.3 m length have been considered but were never implemented.
A 5.4 meter diameter fairing was developed and built by RUAG Space in Switzerland. The RUAG fairing uses carbon fiber composite construction and is based on a similar flight-proven fairing for the Ariane 5. Three configurations are manufactured to support the Atlas V: 20.7 m, 23.4 m, and 26.5 meter long. While the classic 4-meter fairing covers only the payload, the RUAG fairing is much longer and fully encloses both the Centaur upper stage and the payload.

Upgrades

Many systems on the Atlas V have been the subject of upgrade and enhancement both prior to the first Atlas V flight and since that time. Work on a new Fault Tolerant Inertial Navigation Unit started in 2001 to enhance mission reliability for Atlas vehicles by replacing the existing non-redundant navigation and computing equipment with a fault-tolerant unit. The upgraded FTINU first flew in 2006, and in 2010 a follow-on order for more FTINU units was awarded. Later in the decade, the FTINU was replaced with avionics common to both the Atlas V and Delta IV.

Human-rating

Proposals and design work to human-rate the Atlas V began as early as 2006, with ULA's parent company Lockheed Martin reporting an agreement with Bigelow Aerospace that was intended to lead to commercial private trips to low Earth orbit.
Human-rating design and simulation work began in earnest in 2010, with the award of in the first phase of the NASA Commercial Crew Program to develop an Emergency Detection System.
As of February 2011, ULA had received an extension to April 2011 from NASA and was finishing up work on the EDS.
NASA solicited proposals for CCP phase 2 in October 2010, and ULA proposed to complete design work on the EDS. At the time, NASA's goal was to get astronauts to orbit by 2015. Then-ULA President and CEO Michael Gass stated that a schedule acceleration to 2014 was possible if funded. Other than the addition of the Emergency Detection System, no major changes were expected to the Atlas V rocket, but ground infrastructure modifications were planned. The most likely candidate for the human-rating was the N02 configuration, with no fairing, no solid rocket boosters, and dual RL10 engines on the Centaur upper stage.
On 18 July 2011, NASA and ULA announced an agreement on the possibility of certifying the Atlas V to NASA's standards for human spaceflight. ULA agreed to provide NASA with data on the Atlas V, while NASA would provide ULA with draft human certification requirements. In 2011, the human-rated Atlas V was also still under consideration to carry spaceflight participants to the proposed Bigelow Commercial Space Station.
In 2011, Sierra Nevada Corporation picked the Atlas V to be the booster for its still-under-development Dream Chaser crewed spaceplane. The Dream Chaser was intended to launch on an Atlas V, fly a crew to the ISS, and landing horizontally following a lifting-body reentry. However, in late 2014 NASA did not select the Dream Chaser to be one of the two vehicles selected under the Commercial Crew competition.
On 4 August 2011, Boeing announced that it would use the Atlas V as the initial launch vehicle for its CST-100 crew capsule. CST-100 will take NASA astronauts to the International Space Station and was also intended to service the proposed Bigelow Commercial Space Station. A three-flight test program was projected to be completed by 2015, certifying the Atlas V/CST-100 combination for human spaceflight operations. The first flight was expected to include an Atlas V rocket integrated with an uncrewed CST-100 capsule, the second flight an in-flight launch abort system demonstration in the middle of that year, and the third flight a crewed mission carrying two Boeing test-pilot astronauts into LEO and returning them safely at the end of 2015. These plans did not materialize.
In 2014, NASA selected the Boeing CST-100 space capsule as part of the CCD program after extensive delays. Atlas V is the launch vehicle of the CST-100. The first launch of an uncrewed CST-100 capsule occurred atop a human-rated Atlas V on the morning of December 20, 2019, however an anomaly with the Mission Elapsed Time clock aboard the CST-100 caused the spacecraft to enter a suboptimal orbit. As a result, the CST-100 could not achieve orbital insertion to reach the International Space Station, and instead deorbited after two days.

New solid boosters

In 2015, ULA announced that the Aerojet Rocketdyne-produced AJ-60A solid rocket boosters currently in use on Atlas V will be superseded by new GEM 63 boosters produced by Northrop Grumman Innovation Systems. The extended GEM-63XL boosters will also be used on the Vulcan rocket that will replace the Atlas V. The first Atlas V launch with GEM 63 boosters is expected in 2020.

Versions

Each Atlas V booster configuration has a three-digit designation. The first digit shows the diameter of the payload fairing and has a value of "4" or "5" for fairing launches and "N" for crew capsule launches. The second digit indicates the number of solid rocket boosters attached to the base of the rocket and can range from "0" through "3" with the 4-meter fairing, and "0" through "5" with the 5-meter fairing. As seen in the first image, all SRB layouts are asymmetrical. The third digit represents the number of engines on the Centaur stage, either "1" or "2".
For example, an Atlas V 551 has a 5-meter fairing, 5 SRBs, and 1 Centaur engine, whereas an Atlas V 431 has a 4-meter fairing, 3 SRBs, and 1 Centaur engine. The Atlas V N22 with no fairing, two SRBs, and 2 Centaur engines was first launched in 2019. The flight carried the Starliner vehicle for its first orbital test flight.
, all versions of the Atlas V, its design and production rights, and intellectual property rights are owned by ULA and Lockheed Martin.

Capabilities

List date: August 8, 2019 Mass to LEO numbers are at an inclination of 28.5°. Acronyms: Single Engine Centaur, Dual Engine Centaur.
VersionFairingCCBsSRBsUpper stagePayload to LEO, kgPayload to GTO, kgLaunches to dateBase price
4014 m1SEC9,7974,75038$109M
4024 m1DEC12,5000
4114 m11SEC12,1505,9505$115M
4124 m11DEC0
4214 m12SEC14,0676,8907$123M
4224 m12DEC0
4314 m13SEC15,7187,7003$130M
5015.4 m1SEC8,1233,7756$120M
5025.4 m1DEC0
5115.4 m11SEC10,9865,2500 $130M
5125.4 m11DEC0
5215.4 m12SEC13,4906,4752$135M
5225.4 m12DEC0
5315.4 m13SEC15,5757,4753$140M
5325.4 m13DEC0
5415.4 m14SEC17,4438,2906$145M
5425.4 m14DEC0
5515.4 m15SEC18,8148,900
10$153M
5525.4 m15DEC20,5200
Heavy 5.4 m3SEC0
Heavy 5.4 m3DEC29,4000
N22 -12DEC~13,000
1

Launch cost

Before 2016, pricing information for Atlas V launches was limited. In 2010, NASA contracted with ULA to launch the MAVEN mission on an Atlas V 401 for approximately $187 million. The 2013 cost of this configuration for the Air Force under their block buy of 36 rockets was $164 million. In 2015, the TDRS-M launch on an Atlas 401 cost NASA $132.4 million.
Starting in 2016, ULA provided pricing for the Atlas V through its RocketBuilder website, advertising a base price for each rocket configuration, which ranges from $109 million for the 401 up to $153 million for the 551. Each additional SRB adds an average of $6.8 million to the cost of the rocket. Customers can also choose to purchase larger payload fairings or additional launch service options. NASA and Air Force launch costs are often higher than equivalent commercial missions due to additional government accounting, analysis, processing, and mission assurance requirements, which can add $30–$80 million to the cost of a launch.
In 2013, launch costs for commercial satellites to GTO averaged about $100 million, significantly lower than historic Atlas V pricing. However, in recent years the price of an Atlas V has dropped from approximately $180 million to $109 million, in large part due to competitive pressure that emerged in the launch services marketplace during the early 2010s. ULA CEO Tory Bruno has stated that ULA needs at least 2 commercial missions each year in order to stay profitable going forward. ULA is not attempting to win these missions on purely lowest purchase price, stating that it "would rather be the best value provider". ULA suggests that customers will have much lower insurance and delay costs because of the high Atlas V reliability and schedule certainty, making overall customer costs close to that of using competitors like the SpaceX Falcon 9.

Historically proposed versions

In 2006, ULA offered an Atlas V Heavy option that would use three Common Core Booster stages strapped together to lift a 29,400 kg payload to low Earth orbit. ULA stated at the time that 95% of the hardware required for the Atlas V Heavy has already been flown on the Atlas V single-core vehicles. The lifting capability of the proposed rocket was to be roughly equivalent to the Delta IV Heavy, which uses RS-68 engines developed and produced domestically by Aerojet Rocketdyne.
A 2006 report, prepared by the RAND Corporation for the Office of the Secretary of Defense, stated that Lockheed Martin had decided not to develop an Atlas V heavy-lift vehicle. The report recommended for the Air Force and the National Reconnaissance Office to "determine the necessity of an EELV heavy-lift variant, including development of an Atlas V Heavy", and to "resolve the RD-180 issue, including coproduction, stockpile, or U.S. development of an RD-180 replacement".
In 2010, ULA stated that the Atlas V Heavy configuration could be available to customers 30 months from the date of order.
;Atlas V PH2:
In late 2006, the Atlas V program gained access to the tooling and processes for 5-meter-diameter stages used on Delta IV when Boeing and Lockheed Martin space operations were merged into the United Launch Alliance. This led to a proposal to combine the 5 meter diameter Delta IV tankage production processes with dual RD-180 engines, resulting in the Atlas Phase 2.
An Atlas V PH2-Heavy consisting of three 5 m stages in parallel with six RD-180s was considered in the Augustine Report as a possible heavy lifter for use in future space missions, as well as the Shuttle-derived Ares V and Ares V Lite. If built, the Atlas PH2-Heavy was projected to be able to launch a payload mass of approximately 70 metric tons into an orbit of 28.5° inclination.
Neither of the Atlas V Phase 2 proposals progressed to development work.
;Booster for GX rocket:
The Atlas V Common Core Booster was to have been used as the first stage of the joint US-Japanese GX rocket, which was scheduled to make its first flight in 2012. GX launches would have been from the Atlas V launch complex at Vandenberg AFB, SLC-3E. However, the Japanese government decided to cancel the GX project in December 2009.
;Out-licencing rejected by ULA:
In May 2015, a consortium of companies, including Aerojet and Dynetics, sought to license the production or manufacturing rights to the Atlas V using the AR1 engine in place of the RD-180. The proposal was rejected by ULA.

Atlas V launches

Flight No.Date and timeTypeSerial no.Launch sitePayloadType of payloadOrbitOutcomeRemarks
1August 21, 2002
22:05
401AV-001CCAFS SLC-41Hot Bird 6Commercial communications satellite GTOFirst Atlas V launch
2May 13, 2003
22:10
401AV-002CCAFS SLC-41Hellas Sat 2Commercial comsatGTOFirst satellite for Greece and Cyprus
3July 17, 2003
23:45
521AV-003CCAFS SLC-41Rainbow 1Commercial comsatGTOFirst Atlas V 500 launch
First Atlas V launch with SRBs
4December 17, 2004
12:07
521AV-005CCAFS SLC-41AMC 16Commercial comsatGTO
5March 11, 2005
21:42
431AV-004CCAFS SLC-41Inmarsat 4-F1Commercial comsatGTOFirst Atlas V 400 launch with SRBs
6August 12, 2005
11:43
401AV-007CCAFS SLC-41Mars Reconnaissance OrbiterMars orbiterHeliocentric to
Areocentric
First Atlas V launch for NASA
7January 19, 2006
19:00
551AV-010CCAFS SLC-41New HorizonsPluto and Kuiper Belt probeHyperbolicBoeing Star 48B third stage used, first Atlas V launch with a third stage
8April 20, 2006
20:27
411AV-008CCAFS SLC-41Astra 1KRCommercial comsatGTO
9March 9, 2007
03:10
401AV-013CCAFS SLC-41Space Test Program-16 military research satellitesLEO
10June 15, 200715:12401AV-009CCAFS SLC-41USA-194 Two NRO Reconnaissance satellitesLEOFirst Atlas V flight for the National Reconnaissance Office Atlas did not achieve the intended orbit, but payload compensated for shortfall. Customer declared success.
11October 11, 2007
00:22
421AV-011CCAFS SLC-41USA-195 Military comsatGTOValve replacement delayed launch
12December 10, 2007
22:05
401AV-015CCAFS SLC-41USA-198 NRO reconnaissance satelliteMolniya
13March 13, 2008
10:02
411AV-006VAFB SLC-3EUSA-200 NRO reconnaissance satelliteMolniyaFirst Atlas V launch from Vandenberg
14April 14, 2008
20:12
421AV-014CCAFS SLC-41ICO G1Commercial comsatGTO
  • Lockheed Martin Commercial Launch Services launch
  • Heaviest payload launched by an Atlas until the launch of MUOS-1 in 2012.
  • Largest comsat in the world at time of launch until the launch of TerreStar-1 in 2009 by Ariane 5 and then Telstar 19V on July 21, 2018 by Falcon 9.
15April 4, 200900:31421AV-016CCAFS SLC-41USA-204 Military comsatGTO
16June 18, 2009
21:32
401AV-020CCAFS SLC-41LRO/LCROSSLunar explorationHEO to LunarFirst Centaur stage to impact on the Moon.
17September 8, 2009
21:35
401AV-018CCAFS SLC-41USA-207 Military comsatGTOThe Centaur upper stage fragmented in orbit about 24 March 2019
18October 18, 2009
16:12
401AV-017VAFB SLC-3EUSA-210 Military weather satelliteLEO
19November 23, 2009
06:55
431AV-024CCAFS SLC-41Intelsat 14Commercial comsatGTOLMCLS launch
20February 11, 2010
15:23
401AV-021CCAFS SLC-41SDOSolar telescopeGTO
21April 22, 2010
23:52
501AV-012CCAFS SLC-41USA-212 Military orbital test vehicleLEOA piece of the external fairing did not break up on impact, but washed up on Hilton Head Island.
22August 14, 2010
11:07
531AV-019CCAFS SLC-41USA-214 Military comsatGTO
23September 21, 2010
04:03
501AV-025VAFB SLC-3EUSA-215 NRO reconnaissance satelliteLEO
24March 5, 2011
22:46
501AV-026CCAFS SLC-41USA-226 Military orbital test vehicleLEO
25April 15, 2011
04:24
411AV-027VAFB SLC-3EUSA-229 NRO reconnaissance satelliteLEO
26May 7, 2011
18:10
401AV-022CCAFS SLC-41USA-230 Missile Warning satelliteGTO
27August 5, 2011
16:25
551AV-029CCAFS SLC-41JunoJupiter orbiterHyperbolic to
Jovicentric
28November 26, 2011
15:02
541AV-028CCAFS SLC-41Mars Science LaboratoryMars roverHyperbolic
First launch of the 541 configuation
Centaur entered orbit around the sun
29February 24, 2012
22:15
551AV-030CCAFS SLC-41MUOS-1Military comsatGTO
  • 200th Centaur launch
  • Heaviest payload launched by an Atlas until launch of MUOS-2
30May 4, 201218:42531AV-031CCAFS SLC-41USA-235 Military comsatGTO
31June 20, 2012
12:28
401AV-023CCAFS SLC-41USA-236 NRO reconnaissance satelliteGTO50th EELV launch
32August 30, 2012
08:05
401AV-032CCAFS SLC-41Van Allen Probes Van Allen Belts explorationHEO
33September 13, 2012
21:39
401AV-033VAFB SLC-3EUSA-238 NRO reconnaissance satellitesLEO
34December 11, 2012
18:03
501AV-034CCAFS SLC-41USA-240 Military orbital test vehicleLEO
35January 31, 2013
01:48
401AV-036CCAFS SLC-41TDRS-K Data relay satelliteGTO
36February 11, 2013
18:02
401AV-035VAFB SLC-3ELandsat 8Earth Observation satelliteLEOFirst West Coast Atlas V Launch for NASA
37March 19, 2013
21:21
401AV-037CCAFS SLC-41USA-241 Missile Warning satelliteGTO
38May 15, 2013
21:38
401AV-039CCAFS SLC-41USA-242 Navigation satelliteMEO
  • First GPS satellite launched by an Atlas V
  • Longest Atlas V mission to date
39July 19, 201313:00551AV-040CCAFS SLC-41MUOS-2Military comsatGTO
40September 18, 2013
08:10
531AV-041CCAFS SLC-41USA-246 Military comsatGTO
41November 18, 2013
18:28
401AV-038CCAFS SLC-41MAVENMars orbiterHyperbolic to
Areocentric
42December 6, 2013
07:14
501AV-042VAFB SLC-3EUSA-247 NRO reconnaissance satelliteLEO
43January 24, 2014
02:33
401AV-043CCAFS SLC-41TDRS-L Data relay satelliteGTO
44April 3, 2014
14:46
401AV-044VAFB SLC-3EUSA-249 Military weather satelliteLEO50th RD-180 launch
45April 10, 2014
17:45
541AV-045CCAFS SLC-41USA-250 NRO reconnaissance satelliteGTO
46May 22, 2014
13:09
401AV-046CCAFS SLC-41USA-252 NRO reconnaissance satelliteGTO
47August 2, 2014
03:23
401AV-048CCAFS SLC-41USA-256 Navigation satelliteMEO
48August 13, 2014
18:30
401AV-047VAFB SLC-3EWorldView-3Earth imaging satelliteLEO
49September 17, 2014
00:10
401AV-049CCAFS SLC-41USA-257 Military comsatGTOThe Centaur upper stage fragmented on 31 August 2018
50October 29, 2014
17:21
401AV-050CCAFS SLC-41USA-258 Navigation satelliteMEO50th Atlas V launch
51December 13, 2014
03:19
541AV-051VAFB SLC-3EUSA-259 NRO reconnaissance satelliteMolniyaFirst use of the RL-10C engine on the Centaur stage
52January 21, 2015
01:04
551AV-052CCAFS SLC-41MUOS-3Military comsatGTO
53March 13, 2015
02:44
421AV-053CCAFS SLC-41MMSMagnetosphere research satellitesHEO
54May 20, 2015
15:05
501AV-054CCAFS SLC-41USA-261 Military orbital test vehicleLEO
55July 15, 2015
15:36
401AV-055CCAFS SLC-41USA-262 Navigation satelliteMEO
56September 2, 2015
10:18
551AV-056CCAFS SLC-41MUOS-4Military comsatGTO
57October 2, 2015
10:28
421AV-059CCAFS SLC-41Mexsat-2ComsatGTO
58October 8, 2015
12:49
401AV-058VAFB SLC-3EUSA-264 NRO reconnaissance satellitesLEO
59October 31, 2015
16:13
401AV-060CCAFS SLC-41USA-265 Navigation satelliteMEO
60December 6, 2015
21:44
401AV-061CCAFS SLC-41Cygnus CRS OA-4ISS logistics spacecraftLEOFirst Atlas rocket used to directly support the ISS program
61February 5, 2016
13:38
401AV-057CCAFS SLC-41USA-266 Navigation satelliteMEO
62March 23, 2016
03:05
401AV-064CCAFS SLC-41Cygnus CRS OA-6ISS logistics spacecraftLEOFirst stage shut down early but did not affect mission outcome
63June 24, 2016
14:30
551AV-063CCAFS SLC-41MUOS-5Military comsatGTO
64July 28, 2016
12:37
421AV-065CCAFS SLC-41USA-267 NRO reconnaissance satelliteGTO
65September 8, 2016
23:05
411AV-067CCAFS SLC-41OSIRIS-RExAsteroid sample returnHeliocentric
66November 11, 2016
18:30
401AV-062VAFB SLC-3EWorldView-4 + 7 NRO cubesatsEarth Imaging, cubesatsSSOLMCLS launch
67November 19, 2016
23:42
541AV-069CCAFS SLC-41GOES-R MeteorologyGTO100th EELV launch
68December 18, 2016
19:13
431AV-071CCAFS SLC-41EchoStar 19 Commercial comsatGTOLMCLS launch
69January 21, 2017
00:42
401AV-066CCAFS SLC-41USA-273 Missile Warning satelliteGTO
70March 1, 2017
17:49
401AV-068VAFB SLC-3EUSA-274 NRO Reconnaissance SatelliteLEO
71April 18, 2017
15:11
401AV-070CCAFS SLC-41Cygnus CRS OA-7ISS logistics spacecraftLEO
72August 18, 2017
12:29
401AV-074CCAFS SLC-41TDRS-M Data relay satelliteGTO
73September 24, 2017
05:49
541AV-072VAFB SLC-3EUSA-278 NRO Reconnaissance SatelliteMolniya
74October 15, 2017
07:28
421AV-075CCAFS SLC-41USA-279 NRO Reconnaissance satelliteGTO
75January 20, 2018
00:48
411AV-076CCAFS SLC-41USA-282 Missile Warning satelliteGTO
76March 1, 2018
22:02
541AV-077CCAFS SLC-41GOES-S MeteorologyGTOExpended the 100th AJ-60 SRB
77April 14, 2018
23:13
551AV-079CCAFS SLC-41AFSPC-11Military comsatGEO
78May 5, 2018
11:05
401AV-078VAFB SLC-3EInSight MarCOMars lander; 2 CubeSatsHyperbolic
First interplanetary mission from VAFB; first interplanetary CubeSats.
79October 17, 2018,
04:15
551AV-073CCAFS SLC-41USA-288 Military comsatGTO250th Centaur. The Centaur upper stage fragmented in orbit on 6 Apr 2019.
80August 8, 2019,
10:13
551AV-083CCAFS SLC-41USA-292 Military comsatGTO
81December 20, 2019,
11:36
N22AV-080CCAFS SLC-41Starliner Boeing OFTUncrewed orbital test flightSuborbital
LEO
First flight of a Dual-Engine Centaur on Atlas V. First orbital test flight of Starliner. Planned to visit ISS, but an anomaly with the Starliner vehicle left the spacecraft in too low an orbit to do so. The Atlas V rocket performed as expected and thus the mission is listed as successful here.
82February 10, 2020,
04:03
411AV-087CCAFS SLC-41Solar OrbiterSolar heliophysics orbiterHeliocentric
83March 26, 2020,
20:18
551AV-086CCAFS SLC-41AEHF-6Military comsatGTOFirst ever flight for the U.S. Space Force. 500th flight of the RL10 engine
84May 17, 2020,
13:14
501AV-081CCAFS SLC-41USA-299 X-37 military spaceplane; USAFA sat.LEOSixth flight of X-37B; FalconSat-8
85July 30, 2020, 11:50541AV-088CCAFS SLC-41Mars 2020Mars roverHeliocentric

For planned launches, see List of Atlas launches.

Notable missions

The first payload, the Hot Bird 6 communications satellite, was launched to geostationary transfer orbit on 21 August 2002 by an Atlas V 401.
On 12 August 2005, the Mars Reconnaissance Orbiter was launched aboard an Atlas V 401 rocket from Space Launch Complex 41 at Cape Canaveral Air Force Station. The Centaur upper stage of the rocket completed its burns over a 56-minute period and placed MRO into an interplanetary transfer orbit towards Mars
On 19 January 2006, New Horizons was launched by a Lockheed Martin Atlas V 551 rocket. A third stage was added to increase the heliocentric speed. This was the first launch of the Atlas V 551 configuration with five solid rocket boosters, and the first Atlas V with a third stage.
On 6 December 2015, Atlas V lifted its heaviest payload to date into orbit – a Cygnus resupply craft.
On 8 September 2016, the OSIRIS-REx Asteroid Sample Return Mission was launched on an Atlas V 411 rocket. It was scheduled to arrive at the asteroid Bennu in 2018 and return with a sample ranging from 60 grams to 2 kilograms in 2023.
The first four Boeing X-37B spaceplane missions were successfully launched with the Atlas V. The X-37B, also known as the Orbital Test Vehicle, is a reusable robotic spacecraft operated by USAF that can autonomously conduct landings from orbit to a runway. The first four X-37B flights were launched on Atlas V's from Cape Canaveral Air Force Station in Florida with subsequent landings taking place on the Space Shuttle runway located at Vandenberg Air Force Base in California.
On 20 December 2019, the first Starliner crew capsule was launched in Boe-OFT uncrewed test flight. The Atlas V carrier rocket performed flawlessly but an anomaly with the spacecraft left it in a wrong orbit. The orbit was too low to reach the flight's destination of ISS, and the mission was subsequently cut short.

Mission success record

In its 82 launches, starting with its first launch in August 2002, Atlas V has had an almost perfect mission success rate. This is in contrast to the industry failure rate of 5–10%. However, there have been two anomalous flights that – while still successful in their mission – prompted a grounding of the Atlas fleet while investigations determined the root cause of their problems.
The first anomalous event in the use of the Atlas V launch system occurred on June 15, 2007, when the engine in the Centaur upper stage of an Atlas V shut down early, leaving its payload – a pair of NRO L-30 ocean surveillance satellites – in a lower than intended orbit. The cause of the anomaly was traced to a leaky valve, which allowed fuel to leak during the coast between the first and second burns. The resulting lack of fuel caused the second burn to terminate 4 seconds early. Replacing the valve led to a delay in the next Atlas V launch. However, the customer categorized the mission as a success.
A flight on March 23, 2016, suffered an underperformance anomaly on the first-stage burn and shut down 5 seconds early. The Centaur proceeded to boost the Orbital Cygnus payload, the heaviest on an Atlas to date, into the intended orbit by using its fuel reserves to make up for the shortfall from the first stage. This longer burn cut short a later Centaur disposal burn. An investigation of the incident revealed that this anomaly was due to a fault in the main engine mixture-ratio supply valve, which restricted the flow of fuel to the engine. The investigation and subsequent examination of the valves on upcoming missions led to a delay of the next several launches.

Replacement with Vulcan

In 2014, geopolitical and US political considerations led to an effort to replace the Russian-supplied RD-180 engine used on the first-stage booster of the Atlas V. Formal study contracts were issued in June 2014 to a number of US rocket-engine suppliers. The results of those studies have led a decision by ULA to develop the new Vulcan launch vehicle to replace the existing Atlas V and Delta IV.
In September 2014, ULA announced a partnership with Blue Origin to develop the BE-4 LOX/methane engine to replace the RD-180 on a new first-stage booster. As the Atlas V core is designed around RP-1 fuel and cannot be retrofitted to use a methane-fueled engine, a new first stage is being developed. This booster will have the same first-stage tankage diameter as the Delta IV and will be powered by two thrust BE-4 engines. The engine was already in its third year of development by Blue Origin, and ULA expected the new stage and engine to start flying no earlier than 2019.
Vulcan will initially use the same Centaur upper stage as on Atlas V, later to be upgraded to ACES. It will also use a variable number of optional solid rocket boosters, called the GEM 63XL, derived from the new solid boosters planned for Atlas V.
As of 2017, the Aerojet AR1 rocket engine was under development as a backup plan for Vulcan.
, no replacement was expected before mid-2021.

Photo gallery