Antares (rocket)

<h2 id="history">History</h2>
As the <a href="/facts/Space_Shuttle_program/6Ikdvwsw">Space Shuttle program</a> neared its end, NASA sought to develop new capabilities for resupplying the <a href="/facts/International_Space_Station/VNPUBz9m">International Space Station</a> (ISS). Departing from the traditional model of government-owned and operated spacecraft, the agency proposed a new approach: commercial companies would operate spacecraft, while NASA would act as a customer.
To encourage innovation, NASA offered funding through the <a href="/facts/Commercial_Orbital_Transportation_Services/wYMHLjrk">Commercial Orbital Transportation Services</a> (COTS) program to support the development of new spacecraft and launch vehicles. On February 19, 2008, NASA announced that it would award <a href="/facts/Orbital_Sciences_Corporation/WNB0SKlF">Orbital Sciences Corporation</a> a COTS contract worth $171 million. Orbital was expected to invest an additional $150 million, divided between $130 million for the rocket booster and $20 million for the spacecraft.<a class="footnote-ref" id="fnref:2" href="#fn:2">2</a>
As part of the COTS program, Orbital would be expected to conduct a successful demonstration of its rocket booster and spacecraft. If both demonstration flights were successful, Orbital would be eligible for a lucrative <a href="/facts/Commercial_Resupply_Service/TahzTN1Y">Commercial Resupply Service</a> contract of $1.9 billion for eight flights to the ISS.<a class="footnote-ref" id="fnref:3" href="#fn:3">3</a>
In June 2008, it was announced that the <a href="/facts/Mid-Atlantic_Regional_Spaceport/NerIMmk0">Mid-Atlantic Regional Spaceport</a>, formerly part of the <a href="/facts/Wallops_Flight_Facility/F6QvD712">Wallops Flight Facility</a>, in <a href="/facts/Virginia/WSyGxzaH">Virginia</a>, would be the primary launch site for the rocket.<a class="footnote-ref" id="fnref:4" href="#fn:4">4</a> <a href="/facts/Mid-Atlantic_Regional_Spaceport_Launch_Pad_0/tdB0Io71">Launch pad 0A</a> (LP-0A), previously used for the failed <a href="/facts/Conestoga_(rocket)/JvJXyehR">Conestoga</a> rocket, would be modified to handle Antares.<a class="footnote-ref" id="fnref:5" href="#fn:5">5</a> Wallops allows launches which reach the International Space Station's orbit as effectively as those from <a href="/facts/Cape_Canaveral/DsFRGqWm">Cape Canaveral</a>, Florida, while being less crowded.<a class="footnote-ref" id="fnref:6" href="#fn:6">6</a><a class="footnote-ref" id="fnref:7" href="#fn:7">7</a> The first Antares flight launched a Cygnus mass simulator.<a class="footnote-ref" id="fnref:8" href="#fn:8">8</a>
On December 10, 2009, <a href="/facts/Alliant_Techsystems_Inc./zsvwqX5b">Alliant Techsystems Inc.</a> (ATK) test-fired their Castor 30 motor for use on the second stage of the Antares rocket.<a class="footnote-ref" id="fnref:9" href="#fn:9">9</a> In March 2010, Orbital Sciences and <a href="/facts/Aerojet/hlrJsgVF">Aerojet</a> completed test firings of the <a href="/facts/AJ-26/vtf276uF">AJ-26</a> engines.<a class="footnote-ref" id="fnref:10" href="#fn:10">10</a>
Originally designated the Taurus II, Orbital Sciences renamed the vehicle Antares, after the <a href="/facts/Antares/adRhtq7X">star of the same name</a>,<a class="footnote-ref" id="fnref:11" href="#fn:11">11</a> on December 12, 2011.
As of April 2012, development costs were estimated at $472 million.<a class="footnote-ref" id="fnref:12" href="#fn:12">12</a>
On February 22, 2013, a hot fire test was successfully performed, the entire first stage being erected on the pad and held down while the engines fired for 29 seconds.<a class="footnote-ref" id="fnref:13" href="#fn:13">13</a>

<h2 id="design">Design</h2>

<h3>First stage</h3>
The <a href="/facts/Multistage_rocket/WNrmgztj">first stage</a> of Antares burns <a href="/facts/RP-1/wDI7vNdu">RP-1</a> (kerosene) and <a href="/facts/Liquid_oxygen/qnI0KDTb">liquid oxygen</a> (LOX). As Orbital had little experience with large liquid stages and LOX propellant, the first stage core was designed and is manufactured in <a href="/facts/Ukraine/Qof0uqAj">Ukraine</a> by <a href="/facts/KB_Pivdenne/euSxfxsR">Pivdenne Design Office</a> and <a href="/facts/PA_Pivdenmash/lXU5z0xQ">Pivdenmash</a><a class="footnote-ref" id="fnref:14" href="#fn:14">14</a> and includes propellant tanks, pressurization tanks, valves, sensors, feed lines, tubing, wiring and other associated hardware.<a class="footnote-ref" id="fnref:15" href="#fn:15">15</a> Like the <a href="/facts/Zenit_rocket/fkovnBhD">Zenit</a>—also manufactured by Pivdenmash—the Antares vehicle has a diameter of 3.9 m (150 in) with a matching 3.9 m <a href="/facts/Payload_fairing/V1UezFkV">payload fairing</a>.<a class="footnote-ref" id="fnref:16" href="#fn:16">16</a>

<h4>Antares 100 series</h4>
The Antares 100-series first stage was powered by two <a href="/facts/Aerojet/hlrJsgVF">Aerojet</a> <a href="/facts/NK-33/vtf276uF">AJ26</a> engines. These began as <a href="/facts/Kuznetsov_Design_Bureau/FqA5sy93">Kuznetsov</a> <a href="/facts/NK-33/vtf276uF">NK-33</a> engines built in the <a href="/facts/Soviet_Union/m7wWsPto">Soviet Union</a> in the late 1960s and early 1970s, 43 of which were purchased by Aerojet in the 1990s. Twenty of these were refurbished into AJ26 engines for Antares.<a class="footnote-ref" id="fnref:17" href="#fn:17">17</a> Modifications included equipping the engines for <a href="/facts/Gimbal/FI8hEuss">gimballing</a>, adding US electronics, and qualifying the engines to fire for twice as long as designed and to operate at 108% of their original thrust.<a class="footnote-ref" id="fnref:18" href="#fn:18">18</a><a class="footnote-ref" id="fnref:19" href="#fn:19">19</a> Together they produced 3,265 kilonewtons (734,000 lbf) of thrust at sea level and 3,630 kN (816,100 lbf) in vacuum.<a class="footnote-ref" id="fnref:20" href="#fn:20">20</a>
Following the catastrophic failure of an AJ26 during testing at <a href="/facts/Stennis_Space_Center/I0mkeu7L">Stennis Space Center</a> in May 2014 and the <a href="/facts/Cygnus_CRS_Orb-3/Vbyf1zIj">Orb-3</a> launch failure in October 2014, likely caused by an engine turbopump,<a class="footnote-ref" id="fnref:21" href="#fn:21">21</a> the Antares 100-series was retired.

<h4>Antares 200 series</h4>
Because of concerns over corrosion, aging, and the limited supply of AJ26 engines, Orbital had selected new first stage engines<a class="footnote-ref" id="fnref:22" href="#fn:22">22</a><a class="footnote-ref" id="fnref:23" href="#fn:23">23</a> to bid on a <a href="/facts/Commercial_Resupply_Services_2/TahzTN1Y">second major long-term contract</a> for cargo resupply of the <a href="/facts/ISS/VNPUBz9m">ISS</a>. After the loss of the Antares rocket in October 2014, Orbital Sciences announced that the Russian RD-181—a modified version of the <a href="/facts/RD-191/uEko9DN7">RD-191</a>—would replace the AJ-26 on the Antares 200-series.<a class="footnote-ref" id="fnref:24" href="#fn:24">24</a><a class="footnote-ref" id="fnref:25" href="#fn:25">25</a> The first flight of the Antares 230 configuration using the RD-181 launched on October 17, 2016, carrying the <a href="/facts/Cygnus_OA-5/jgHDJAG1">Cygnus OA-5</a> cargo to the <a href="/facts/ISS/VNPUBz9m">ISS</a>.
The Antares 200 and 200+ first stages are powered by two RD-181 engines, which provide 440 kilonewtons (100,000 lbf) more thrust than the dual AJ26 engines used on the Antares 100. Orbital adapted the existing core stage to accommodate the increased performance in the 200 Series, allowing Antares to deliver up to 6,500 kg (14,300 lb) to low Earth orbit.<a class="footnote-ref" id="fnref:26" href="#fn:26">26</a> The surplus performance of the Antares 200-series will allow Orbital to fulfill its ISS resupply contract in only four additional flights, rather than the five that would have been required with the Antares 100-series.<a class="footnote-ref" id="fnref:27" href="#fn:27">27</a><a class="footnote-ref" id="fnref:28" href="#fn:28">28</a><a class="footnote-ref" id="fnref:29" href="#fn:29">29</a>
While the 200 series adapted the originally ordered 100 Series stages (<a href="/facts/KB_Pivdenne/euSxfxsR">KB Pivdenne</a>/<a href="/facts/PA_Pivdenmash/lXU5z0xQ">Pivdenmash</a>, Zenit derived),<a class="footnote-ref" id="fnref:30" href="#fn:30">30</a> it requires under-throttling the RD-181 engines, which reduces performance.<a class="footnote-ref" id="fnref:31" href="#fn:31">31</a>
The Antares was upgraded to the Antares 230+ for the NASA Commercial Resupply Services 2 contract. NG-12, launched November 2, 2019, was the first NASA CRS-2 mission to ISS using the 230+ upgrades. The most significant upgrades were structural changes to the intertank bay (between the LOX and RP-1 tanks) and the forward bay (forward of the LOX). Additionally, the company is working on trajectory improvements via a "load-release autopilot" that will provide greater mass to orbit capability.<a class="footnote-ref" id="fnref:32" href="#fn:32">32</a>

<h4>Antares 300 series</h4>
In August 2022, Northrop Grumman announced that it had contracted <a href="/facts/Firefly_Aerospace/4ezytxxr">Firefly Aerospace</a> to build the 300-series first stage, which is similar to their collaborating in-development MLV launch vehicle, and features the same composite structures as well as seven <a href="/facts/Miranda_(engine)/4ezytxxr">Miranda</a> engines producing 7,200 kN (1,600,000 lbf) of thrust—substantially greater than the previous 200-series first stage. Northrop Grumman states that the new first stage substantially increases the mass capability of Antares.<a class="footnote-ref" id="fnref:33" href="#fn:33">33</a><a class="footnote-ref" id="fnref:34" href="#fn:34">34</a>
The announcement occurred as a result of the <a href="/facts/2022_Russian_invasion_of_Ukraine/TTeQCgSl">2022 Russian invasion of Ukraine</a>, which has jeopardized supply chains for the previous first stages, which are manufactured in Ukraine and use <a href="/facts/RD-191/uEko9DN7">RD-181</a> engines from Russia.<a class="footnote-ref" id="fnref:35" href="#fn:35">35</a>

<h3>Second stage</h3>
The second stage is an Orbital ATK <a href="/facts/Castor_(rocket_stage)/D3vgsyc7">Castor 30</a>-series <a href="/facts/Solid-fuel_rocket/RpgdYKIU">solid-fuel rocket</a>, developed as a derivative of the Castor 120 solid motor used as <a href="/facts/Minotaur-C/XQDB2hca">Minotaur-C</a>'s first stage, itself based on a <a href="/facts/LGM-118_Peacekeeper/HpETRcB9">LGM-118 Peacekeeper</a> ICBM first stage.<a class="footnote-ref" id="fnref:36" href="#fn:36">36</a> The first two flights of Antares used a Castor 30A, which was replaced by the enhanced Castor 30B for subsequent flights. The Castor 30B produces 293.4 kN (65,960 lbf) average and 395.7 kN (88,960 lbf) maximum thrust, and uses <a href="/facts/Electromechanical/0D5gkXko">electromechanical</a> <a href="/facts/Thrust_vectoring/B0KeV8Wu">thrust vector</a> control.<a class="footnote-ref" id="fnref:37" href="#fn:37">37</a> For increased performance, the larger Castor 30XL is available<a class="footnote-ref" id="fnref:38" href="#fn:38">38</a> and will be used on ISS resupply flights to allow Antares to carry the Enhanced Cygnus.<a class="footnote-ref" id="fnref:39" href="#fn:39">39</a><a class="footnote-ref" id="fnref:40" href="#fn:40">40</a><a class="footnote-ref" id="fnref:41" href="#fn:41">41</a>
The Castor 30XL upper stage for Antares 230+ is being optimized for the CRS-2 contract. The initial design of the Castor 30XL was conservatively built, and after gaining flight experience it was determined that the structural component of the motor case could be lightened.<a class="footnote-ref" id="fnref:42" href="#fn:42">42</a>

<h3>Third stage</h3>
Antares offers three optional third stages: the Bi-Propellant Third Stage (BTS), a <a href="/facts/Star_48/FrTEvI2K">Star 48</a>-based third stage and an <a href="/facts/Orion_38/pWolsTGj">Orion 38</a> motor. BTS is derived from Orbital's <a href="/facts/GEOStar/E741hGfP">GEOStar</a>, a <a href="/facts/Spacecraft_bus/UMlFYAUY">spacecraft bus</a> and uses <a href="/facts/Nitrogen_tetroxide/01WfnHJh">nitrogen tetroxide</a> and <a href="/facts/Hydrazine/G7P5ITzU">hydrazine</a> for propellant; it is intended to precisely place payloads into their final orbits.<a class="footnote-ref" id="fnref:43" href="#fn:43">43</a> The Star 48-based stage uses a <a href="/facts/Star_48/FrTEvI2K">Star 48BV</a> solid rocket motor and would be used for higher energy orbits.<a class="footnote-ref" id="fnref:44" href="#fn:44">44</a> The Orion 38 is used on the Minotaur and Pegasus rockets as an upper stage.<a class="footnote-ref" id="fnref:45" href="#fn:45">45</a>

<h3>Fairing</h3>
The 3.9-meter (13 ft) diameter, 9.9-meter (32 ft) high <a href="/facts/Payload_fairing/V1UezFkV">fairing</a> is manufactured by Northrop Grumman of <a href="/facts/Iuka%2c_Mississippi/H0XNXsV1">Iuka, Mississippi</a>, which also builds other composite structures for the vehicle, including the combined fairing adapter, dodecagon, motor cone, and interstage.<a class="footnote-ref" id="fnref:46" href="#fn:46">46</a>

<h3>NASA Commercial Resupply Services-2 : Enhancements</h3>
On January 14, 2016, NASA awarded three cargo contracts via CRS-2. Orbital ATK's Cygnus was one of these contracts.<a class="footnote-ref" id="fnref:47" href="#fn:47">47</a>
According to Mark Pieczynski, Orbital ATK Vice President, Flight Systems Group, "A further improved version [of Antares for CRS-2 contract] is in development which will include: Stage 1 core updates including structural reinforcements and optimization to accommodate increased loads. (Also) certain refinements to the RD-181 engines and CASTOR 30XL motor; and Payload accommodations improvements including a 'pop-top' feature incorporated in the fairing to allow late Cygnus cargo load and optimized fairing adapter structure".
Previously, it was understood that these planned upgrades from the Antares 230 series would create a vehicle known as the Antares 300 series. However, when asked specifically about Antares 300 series development, Mr. Pieczynski stated that Orbital ATK has "not determined to call the upgrades, we are working on, a 300 series. This is still TBD".<a class="footnote-ref" id="fnref:48" href="#fn:48">48</a>
In May 2018, the Antares program manager Kurt Eberly indicated that the upgrades will be referred to as Antares 230+.<a class="footnote-ref" id="fnref:49" href="#fn:49">49</a>

<h2 id="configurations-and-numbering">Configurations and numbering</h2>

The first two test flights used a <a href="/facts/Castor_(rocket_stage)/D3vgsyc7">Castor 30A</a> second stage. All subsequent flights will use either a <a href="/facts/Castor_(rocket_stage)/D3vgsyc7">Castor 30B</a> or <a href="/facts/Castor_(rocket_stage)/D3vgsyc7">Castor 30XL</a>. The rocket's configuration is indicated by a three-digit number, the first number representing the first stage, the second the type of second stage, and the third the type of third stage.<a class="footnote-ref" id="fnref:50" href="#fn:50">50</a> A + sign added as suffix (fourth position) signifies performance upgrades to the Antares 230 variant.

<table><tbody><tr><th rowspan="2">Number</th><th>First digit</th><th>Second digit</th><th>Third digit</th></tr><tr><th>(First stage)</th><th>(Second stage)</th><th>(Third stage)</th></tr><tr><th>0</th><td>—</td><td>—</td><td>No third stage</td></tr><tr><th>1</th><td>2 × <a href="/facts/NK-33/vtf276uF">AJ26-62</a></td><td><a href="/facts/Castor_(rocket_stage)/D3vgsyc7">Castor 30A</a></td><td>BTS (3 × <a href="/facts/BT-4_(rocket_engine)/KHdEs53X">BT-4</a>)</td></tr><tr><th>2</th><td>2 × <a href="/facts/RD-181/uEko9DN7">RD-181</a></td><td><a href="/facts/Castor_(rocket_stage)/D3vgsyc7">Castor 30B</a></td><td><a href="/facts/Star_48/FrTEvI2K">Star 48BV</a></td></tr><tr><th>3</th><td>7 × <a href="/facts/Miranda_(engine)/4ezytxxr">Miranda</a></td><td><a href="/facts/Castor_(rocket_stage)/D3vgsyc7">Castor 30XL</a></td><td><a href="/facts/Orion_(rocket_stage)/pWolsTGj">Orion 38</a></td></tr></tbody></table>
<h2 id="notable-missions-and-anomalies">Notable missions and anomalies</h2>
<h3>Antares A-ONE</h3>
Main article: <a href="/facts/Antares_A-ONE/nsEwkK4X">Antares A-ONE</a>
Originally scheduled for 2012, the first Antares launch, designated A-ONE<a class="footnote-ref" id="fnref:51" href="#fn:51">51</a> was conducted on April 21, 2013,<a class="footnote-ref" id="fnref:52" href="#fn:52">52</a> carrying the <a href="/facts/Antares_A-ONE/nsEwkK4X">Cygnus Mass Simulator</a> (a <a href="/facts/Boilerplate_(spaceflight)/eJ4BBdAN">boilerplate</a> <a href="/facts/Cygnus_(spacecraft)/8jFp6gs7">Cygnus spacecraft</a>) and four <a href="/facts/CubeSat/jL2IpYKd">CubeSats</a> contracted by Spaceflight Incorporated: <a href="/facts/Dove_1/IF1z08vV">Dove 1</a> for <a href="/facts/Planet_Labs/IF1z08vV">Cosmogia Incorporated</a> (now Planet Labs) and three <a href="/facts/PhoneSat/H86Xbuwt">PhoneSat</a> satellites—<a href="/facts/Alexander_(satellite)/1WMkbKV9">Alexander</a>,<a class="footnote-ref" id="fnref:53" href="#fn:53">53</a> <a href="/facts/Graham_(satellite)/JIn99Nwp">Graham</a> and <a href="/facts/Bell_(satellite)/VYIEg0D8">Bell</a> for NASA.<a class="footnote-ref" id="fnref:54" href="#fn:54">54</a>
Prior to the launch, a 27-second test firing of the rocket's AJ26 engines was conducted successfully on February 22, 2013, following an attempt on February 13 which was abandoned before ignition.<a class="footnote-ref" id="fnref:55" href="#fn:55">55</a>
A-ONE used the Antares 110 configuration, with a Castor 30A second stage and no third stage. The launch took place from <a href="/facts/Mid-Atlantic_Regional_Spaceport_Launch_Pad_0/tdB0Io71">Pad 0A</a> of the <a href="/facts/Mid-Atlantic_Regional_Spaceport/NerIMmk0">Mid-Atlantic Regional Spaceport</a> on <a href="/facts/Wallops_Island/t5o5CkhD">Wallops Island</a>, <a href="/facts/Virginia/WSyGxzaH">Virginia</a>. LP-0A was a former <a href="/facts/Conestoga_(rocket)/JvJXyehR">Conestoga</a> launch complex which had only been used once before, in 1995, for the Conestoga's only orbital launch attempt.<a class="footnote-ref" id="fnref:56" href="#fn:56">56</a> Antares became the largest—and first—liquid-fuelled rocket to fly from Wallops Island, as well as the largest rocket launched by Orbital Sciences.<a class="footnote-ref" id="fnref:57" href="#fn:57">57</a>
The first attempt to launch the rocket, on April 17, 2013, was scrubbed after an umbilical detached from the rocket's second stage, and a second attempt on April 20 was scrubbed due to high altitude winds.<a class="footnote-ref" id="fnref:58" href="#fn:58">58</a> At the third attempt on April 21, the rocket lifted off at the beginning of its launch window. The launch window for all three attempts was three hours beginning at 21:00 <a href="/facts/Coordinated_Universal_Time/2EnjfSyu">UTC</a> (17:00 <a href="/facts/Eastern_Time_Zone/jP4S8j1V">EDT</a>), shortening to two hours at the start of the terminal count, and ten minutes later in the count.<a class="footnote-ref" id="fnref:59" href="#fn:59">59</a><a class="footnote-ref" id="fnref:60" href="#fn:60">60</a>

<h3>Cygnus CRS Orb-3</h3>
Main article: <a href="/facts/Cygnus_Orb-3/Vbyf1zIj">Cygnus Orb-3</a>

On October 28, 2014, the attempted launch of an Antares carrying a <a href="/facts/Cygnus_(spacecraft)/8jFp6gs7">Cygnus</a> cargo spacecraft on the <a href="/facts/Cygnus_Orb-3/Vbyf1zIj">Orb-3</a> resupply mission failed catastrophically six seconds after liftoff from <a href="/facts/Mid-Atlantic_Regional_Spaceport/NerIMmk0">Mid-Atlantic Regional Spaceport</a> at <a href="/facts/Wallops_Flight_Facility/F6QvD712">Wallops Flight Facility</a>, <a href="/facts/Virginia/WSyGxzaH">Virginia</a>.<a class="footnote-ref" id="fnref:61" href="#fn:61">61</a> An explosion occurred in the thrust section just as the vehicle cleared the tower, and it fell back down onto the launch pad. The range safety officer sent the destruct command just before impact.<a class="footnote-ref" id="fnref:62" href="#fn:62">62</a><a class="footnote-ref" id="fnref:63" href="#fn:63">63</a> There were no injuries.<a class="footnote-ref" id="fnref:64" href="#fn:64">64</a> Orbital Sciences reported that <a href="/facts/Mid-Atlantic_Regional_Spaceport_Launch_Pad_0/tdB0Io71">Launch Pad 0A</a> "escaped significant damage",<a class="footnote-ref" id="fnref:65" href="#fn:65">65</a> though initial estimates for repairs were in the $20 million range.<a class="footnote-ref" id="fnref:66" href="#fn:66">66</a> Orbital Sciences formed an anomaly investigation board to investigate the cause of the incident. They traced it to a failure of the first stage LOX turbopump, but could not find a specific cause. However, the refurbished NK-33 engines, originally manufactured over 40 years earlier and stored for decades, were suspected as having leaks, corrosion, or manufacturing defects that had not been detected.<a class="footnote-ref" id="fnref:67" href="#fn:67">67</a> The NASA Accident Investigation Report was more direct in its failure assessment.<a class="footnote-ref" id="fnref:68" href="#fn:68">68</a> On October 6, 2015, almost one year after the accident, Pad 0A was restored to use. Total repair costs were about $15 million.<a class="footnote-ref" id="fnref:69" href="#fn:69">69</a>
Following the failure, Orbital sought to purchase launch services for its Cygnus spacecraft in order to satisfy its cargo contract with NASA,<a class="footnote-ref" id="fnref:70" href="#fn:70">70</a> and on December 9, 2014, Orbital announced that at least one, and possibly two, Cygnus flights would be launched on <a href="/facts/Atlas_V/5SNgegyt">Atlas V</a> rockets from <a href="/facts/Cape_Canaveral_Air_Force_Station/dwJ9MCPH">Cape Canaveral Air Force Station</a>.<a class="footnote-ref" id="fnref:71" href="#fn:71">71</a> As it happened, <a href="/facts/Cygnus_OA-4/HtLyNnDa">Cygnus OA-4</a> and <a href="/facts/Cygnus_OA-6/xNGIoBdF">Cygnus OA-6</a> were launched with an Atlas V and the Antares 230 performed its maiden flight with <a href="/facts/Cygnus_OA-5/jgHDJAG1">Cygnus OA-5</a> in October 2016. One further mission was launched aboard an Atlas in April 2017 (<a href="/facts/Cygnus_OA-7/dPd7w0ge">Cygnus OA-7</a>), fulfilling Orbital's contractual obligations towards NASA. It was followed by the Antares 230 in regular service with <a href="/facts/Cygnus_OA-8E/72UG1Ykk">Cygnus OA-8E</a> in November 2017, with three further missions scheduled on their extended contract.

<h2 id="launch-statistics">Launch statistics</h2>
This section is transcluded from <a href="/facts/List_of_Antares_launches/G3lHnW9V">List of Antares launches</a>. (<a href="https://en.wikipedia.org/w/index.php?title=List_of_Antares_launches&action=edit">edit</a> | <a href="https://en.wikipedia.org/w/index.php?title=List_of_Antares_launches&action=history">history</a>)

<h3> Rocket configurations</h3>

<ul><li>  Antares 110</li>
<li>  Antares 120</li>
<li>  Antares 130</li>
<li>  Antares 230</li>
<li>  Antares 230+</li></ul>

<h3> Launch outcomes</h3>

2013

'14

'15

'16

'17

'18

'19

'20

'21

'22

'23

'24

'25

'26

<ul><li>  Failure</li>
<li>  Partial failure</li>
<li>  Success</li>
<li>  Scheduled</li></ul>

<h3> Operator</h3>

2013

'14

'15

'16

'17

'18

'19

'20

'21

'22

'23

<ul><li>  <a href="/facts/Orbital_Sciences_Corporation/WNB0SKlF">Orbital Sciences</a></li>
<li>  <a href="/facts/Orbital_ATK/zwkJhWEe">Orbital ATK</a></li>
<li>  <a href="/facts/Northrop_Grumman/M6keKE1A">Northrop Grumman</a></li></ul>

<h2 id="launch-history">Launch history</h2>
This section is transcluded from <a href="/facts/List_of_Antares_launches/G3lHnW9V">List of Antares launches</a>. (<a href="https://en.wikipedia.org/w/index.php?title=List_of_Antares_launches&action=edit">edit</a> | <a href="https://en.wikipedia.org/w/index.php?title=List_of_Antares_launches&action=history">history</a>)

<table><tbody><tr><th scope="col">Flight No.</th><th scope="col">Date / time (<a href="/facts/Coordinated_Universal_Time/2EnjfSyu">UTC</a>)</th><th scope="col">Rocket variant</th><th scope="col">Launch site</th><th scope="col">Payload, Spacecraft name</th><th scope="col">Payload mass</th><th scope="col">Orbit</th><th scope="col">Operator</th><th scope="col">Customer</th><th scope="col">Launch outcome</th></tr><tr><th scope="row" rowspan="2">1</th><td>April 21, 201321:00</td><td>Antares 110</td><td><a href="/facts/Mid-Atlantic_Regional_Spaceport/NerIMmk0">MARS</a>, <a href="/facts/Mid-Atlantic_Regional_Spaceport_Launch_Pad_0/tdB0Io71">LP-0A</a></td><td><ul><li><a href="/facts/Cygnus_Mass_Simulator/nsEwkK4X">Cygnus Mass Simulator</a></li><li><a href="/facts/Dove_(satellite)/IF1z08vV">Dove 1</a></li><li><a href="/facts/Alexander_(satellite)/1WMkbKV9">Alexander</a></li><li><a href="/facts/Graham_(satellite)/JIn99Nwp">Graham</a></li><li><a href="/facts/Bell_(satellite)/VYIEg0D8">Bell</a></li></ul></td><td>—</td><td><a href="/facts/Low_Earth_orbit/rq1TwayJ">LEO</a></td><td><a href="/facts/Orbital_Sciences_Corporation/WNB0SKlF">Orbital Sciences Corporation</a></td><td><a href="/facts/NASA/TIMCV0yV">NASA</a> (<a href="/facts/Commercial_Orbital_Transportation_Services/wYMHLjrk">COTS</a>)</td><td>Success</td></tr><tr><td colspan="9"><a href="/facts/Antares_A-ONE/nsEwkK4X">Antares A-ONE</a>, Antares test flight, using a Castor 30A second stage and no third stage.<a class="footnote-ref" id="fnref:72" href="#fn:72">72</a><a class="footnote-ref" id="fnref:73" href="#fn:73">73</a></td></tr><tr><th scope="row" rowspan="2">2</th><td>September 18, 201314:58</td><td>Antares 110</td><td>MARS, LP-0A</td><td><a href="/facts/Cygnus_(spacecraft)/8jFp6gs7">Cygnus</a> (standard)<a href="/facts/Orb-D1/0NpkWGaj">Orb-D1</a><a href="/facts/G._David_Low/0qEKluWT">G. David Low</a><a class="footnote-ref" id="fnref:74" href="#fn:74">74</a></td><td>700 kg(1,543 lb)<a class="footnote-ref" id="fnref:75" href="#fn:75">75</a></td><td>LEO (<a href="/facts/ISS/VNPUBz9m">ISS</a>)</td><td>Orbital Sciences Corporation</td><td>NASA (COTS)</td><td>Success</td></tr><tr><td colspan="9">Orbital Sciences COTS demonstration flight. First Antares mission with a real Cygnus capsule, first mission to rendezvous and berth with the <a href="/facts/International_Space_Station/VNPUBz9m">International Space Station</a>, second launch of Antares. The rendezvous maneuver was delayed due to a computer data link problem,<a class="footnote-ref" id="fnref:76" href="#fn:76">76</a> but the issue was resolved and berthing followed shortly thereafter.<a class="footnote-ref" id="fnref:77" href="#fn:77">77</a><a class="footnote-ref" id="fnref:78" href="#fn:78">78</a></td></tr><tr><th scope="row" rowspan="2">3</th><td>January 9, 201418:07</td><td>Antares 120</td><td>MARS, LP-0A</td><td>Cygnus (standard)<a href="/facts/CRS_Orb-1/Sd3s6XYa">CRS Orb-1</a><a href="/facts/C._Gordon_Fullerton/HepbKFqT">C. Gordon Fullerton</a><a class="footnote-ref" id="fnref:79" href="#fn:79">79</a></td><td>1,260 kg(2,780 lb)<a class="footnote-ref" id="fnref:80" href="#fn:80">80</a></td><td>LEO (ISS)</td><td>Orbital Sciences Corporation</td><td>NASA (<a href="/facts/Commercial_Resupply_Services/TahzTN1Y">CRS</a>)</td><td>Success</td></tr><tr><td colspan="9">First Commercial Resupply Service (CRS) mission for Cygnus, and first Antares launch using the Castor 30B upper stage.<a class="footnote-ref" id="fnref:81" href="#fn:81">81</a><a class="footnote-ref" id="fnref:82" href="#fn:82">82</a></td></tr><tr><th scope="row" rowspan="2">4</th><td>July 13, 201416:52</td><td>Antares 120</td><td>MARS, LP-0A</td><td>Cygnus (standard)<a href="/facts/CRS_Orb-2/dNB5RCJF">CRS Orb-2</a><a href="/facts/Janice_Voss/rnWMQkA4">Janice Voss</a><a class="footnote-ref" id="fnref:83" href="#fn:83">83</a></td><td>1,494 kg(3,293 lb)<a class="footnote-ref" id="fnref:84" href="#fn:84">84</a></td><td>LEO (ISS)</td><td>Orbital Sciences Corporation</td><td>NASA (CRS)</td><td>Success</td></tr><tr><td colspan="9">Spacecraft carried supplies for the ISS, including research equipment, crew provisions, hardware, and science experiments.<a class="footnote-ref" id="fnref:85" href="#fn:85">85</a></td></tr><tr><th scope="row" rowspan="2">5</th><td>October 28, 201422:22</td><td>Antares 130</td><td>MARS, LP-0A</td><td>Cygnus (standard)<a href="/facts/CRS_Orb-3/Vbyf1zIj">CRS Orb-3</a><a href="/facts/Deke_Slayton/Lc71Aylj">Deke Slayton</a><a class="footnote-ref" id="fnref:86" href="#fn:86">86</a></td><td>2,215 kg(4,883 lb)<a class="footnote-ref" id="fnref:87" href="#fn:87">87</a></td><td>LEO (ISS)</td><td>Orbital Sciences Corporation</td><td>NASA (CRS)</td><td>Failure</td></tr><tr><td colspan="9">LOX turbopump failure T+6 seconds. Rocket fell back onto the pad and exploded.<a class="footnote-ref" id="fnref:88" href="#fn:88">88</a><a class="footnote-ref" id="fnref:89" href="#fn:89">89</a><a class="footnote-ref" id="fnref:90" href="#fn:90">90</a> First Antares launch to use Castor 30XL upper stage. In addition to ISS supplies, payload included a <a href="/facts/Planetary_Resources/QoA54et8">Planetary Resources</a> <a href="/facts/Arkyd-3/QoA54et8">Arkyd-3</a> satellite<a class="footnote-ref" id="fnref:91" href="#fn:91">91</a> and a NASA <a href="/facts/JPL/zPXnxRBf">JPL</a>/<a href="/facts/UT_Austin/6NApstxT">UT Austin</a> CubeSat mission named RACE.<a class="footnote-ref" id="fnref:92" href="#fn:92">92</a></td></tr><tr><th scope="row" rowspan="2">6</th><td>October 17, 201623:45</td><td>Antares 230</td><td>MARS, LP-0A</td><td>Cygnus (enhanced)<a href="/facts/CRS_OA-5/jgHDJAG1">CRS OA-5</a><a href="/facts/Alan_G._Poindexter/ouajMIpT">Alan G. Poindexter</a><a class="footnote-ref" id="fnref:93" href="#fn:93">93</a></td><td>2,425 kg(5,346 lb)<a class="footnote-ref" id="fnref:94" href="#fn:94">94</a></td><td>LEO (ISS)</td><td><a href="/facts/Orbital_ATK/zwkJhWEe">Orbital ATK</a></td><td>NASA (CRS)</td><td>Success</td></tr><tr><td colspan="9">First launch of Enhanced Cygnus on Orbital's new Antares 230.<a class="footnote-ref" id="fnref:95" href="#fn:95">95</a><a class="footnote-ref" id="fnref:96" href="#fn:96">96</a><a class="footnote-ref" id="fnref:97" href="#fn:97">97</a><a class="footnote-ref" id="fnref:98" href="#fn:98">98</a></td></tr><tr><th scope="row" rowspan="2">7</th><td>November 12, 201712:19</td><td>Antares 230</td><td>MARS, LP-0A</td><td>Cygnus (enhanced)<a href="/facts/CRS_OA-8E/72UG1Ykk">CRS OA-8E</a><a href="/facts/Gene_Cernan/yePYCwlv">Gene Cernan</a><a class="footnote-ref" id="fnref:99" href="#fn:99">99</a></td><td>3,338 kg(7,359 lb)<a class="footnote-ref" id="fnref:100" href="#fn:100">100</a></td><td>LEO (ISS)</td><td>Orbital ATK</td><td>NASA (CRS)</td><td>Success</td></tr><tr><td colspan="9"></td></tr><tr><th scope="row" rowspan="2">8</th><td>May 21, 201808:44</td><td>Antares 230</td><td>MARS, LP-0A</td><td>Cygnus (enhanced)<a href="/facts/CRS_OA-9E/W4502KAX">CRS OA-9E</a><a href="/facts/James_R._Thompson_Jr./ISoIX2kL">J.R. Thompson</a><a class="footnote-ref" id="fnref:101" href="#fn:101">101</a></td><td>3,350 kg(7,386 lb)<a class="footnote-ref" id="fnref:102" href="#fn:102">102</a></td><td>LEO (ISS)</td><td>Orbital ATK</td><td>NASA (CRS)</td><td>Success</td></tr><tr><td colspan="9">Spacecraft carried ISS hardware, crew supplies, and scientific payloads, including the Cold Atom Lab and the Biomolecule Extraction and Sequencing Technology experiment.<a class="footnote-ref" id="fnref:103" href="#fn:103">103</a> The Cygnus also demonstrated boosting the station's orbital velocity for the first time, by 0.06 meter per second.<a class="footnote-ref" id="fnref:104" href="#fn:104">104</a></td></tr><tr><th scope="row" rowspan="2">9</th><td>November 17, 201809:01</td><td>Antares 230</td><td>MARS, LP-0A</td><td>Cygnus (enhanced)<a href="/facts/Cygnus_NG-10/YkV7VfCs">CRS NG-10</a><a href="/facts/John_Young_(astronaut)/gD9fX5yr">John Young</a></td><td>3,416 kg(7,531 lb)</td><td>LEO (ISS)</td><td><a href="/facts/Northrop_Grumman/M6keKE1A">Northrop Grumman</a></td><td>NASA (CRS)</td><td>Success</td></tr><tr><td colspan="9">Largest number of satellites launched on a single rocket (108). Cygnus NG-10, CHEFsat 2, <a href="/facts/KickSat/gGcb7seb">Kicksat 2</a>, 104 Sprite Chipsats (deployed from <a href="/facts/KickSat/gGcb7seb">Kicksat 2</a>), MYSAT 1.</td></tr><tr><th scope="row" rowspan="2">10</th><td>April 17, 201920:46</td><td>Antares 230</td><td>MARS, LP-0A</td><td>Cygnus (enhanced)<a href="/facts/Cygnus_NG-11/ENVysndq">CRS NG-11</a><a href="/facts/Roger_B._Chaffee/lVfnH3t4">Roger Chaffee</a><a class="footnote-ref" id="fnref:105" href="#fn:105">105</a></td><td>3,447 kg (7,600 lbs)</td><td>LEO (ISS)</td><td>Northrop Grumman</td><td>NASA (CRS)</td><td>Success</td></tr><tr><td colspan="9">Launched the last mission under the <a href="/facts/Commercial_Resupply_Services/TahzTN1Y">Commercial Resupply Services-1</a> for Cygnus.<a class="footnote-ref" id="fnref:106" href="#fn:106">106</a></td></tr><tr><th scope="row" rowspan="2">11</th><td>November 2, 201913:59</td><td>Antares 230+</td><td>MARS, LP-0A</td><td>Cygnus (enhanced)<a href="/facts/Cygnus_NG-12/eoPsbUF1">CRS NG-12</a><a href="/facts/Alan_Bean/dRLtsPvD">Alan Bean</a><a class="footnote-ref" id="fnref:107" href="#fn:107">107</a></td><td>3,728 kg (8,221 lbs)</td><td>LEO (ISS)</td><td>Northrop Grumman</td><td>NASA (CRS)</td><td>Success</td></tr><tr><td colspan="9">Cygnus NG-12 is the first mission under the NASA <a href="/facts/Commercial_Resupply_Services/TahzTN1Y">Commercial Resupply Services-2</a> contract. NG-12 is also the first to use upgraded launcher, Antares 230+.</td></tr><tr><th scope="row" rowspan="2">12</th><td>February 15, 202020:21</td><td>Antares 230+</td><td>MARS, LP-0A</td><td>Cygnus (enhanced)<a href="/facts/Cygnus_NG-13/TyD3WNQB">CRS NG-13</a><a href="/facts/Robert_Henry_Lawrence_Jr./pzUd7N5f">Robert Lawrence, Jr.</a></td><td>3,377 kg (7,445 lbs)</td><td>LEO (ISS)</td><td>Northrop Grumman</td><td>NASA (CRS)</td><td>Success</td></tr><tr><td colspan="9"></td></tr><tr><th scope="row" rowspan="2">13</th><td>October 3, 202001:16</td><td>Antares 230+</td><td>MARS, LP-0A</td><td>Cygnus (enhanced)<a href="/facts/Cygnus_NG-14/7NCALp42">CRS NG-14</a><a href="/facts/Kalpana_Chawla/l5EY7wmM">Kalpana Chawla</a></td><td>3,458 kg (7,624 lbs)<a class="footnote-ref" id="fnref:108" href="#fn:108">108</a></td><td>LEO (ISS)</td><td>Northrop Grumman</td><td>NASA (CRS)</td><td>Success</td></tr><tr><td colspan="9">Spacecraft carried ISS hardware, crew supplies, and scientific payloads, including a new toilet (Universal Waste Management System, UWMS), Ammonia Electrooxidation, radishes for Plant Habitat-02, drugs for targeted cancer treatments with Onco-Selectors, and a customized 360-degree camera to capture future spacewalks.<a class="footnote-ref" id="fnref:109" href="#fn:109">109</a><a class="footnote-ref" id="fnref:110" href="#fn:110">110</a></td></tr><tr><th scope="row" rowspan="2">14</th><td>February 20, 202117:36</td><td>Antares 230+</td><td>MARS, LP-0A</td><td>Cygnus (enhanced)<a href="/facts/Cygnus_NG-15/WSbvjWmg">CRS NG-15</a><a href="/facts/Katherine_Johnson/NDHKRuMs">Katherine Johnson</a></td><td>3,810 kg (8399 lbs)<a class="footnote-ref" id="fnref:111" href="#fn:111">111</a></td><td>LEO (ISS)</td><td>Northrop Grumman</td><td>NASA (CRS)</td><td>Success</td></tr><tr><td colspan="9">This mission carried over 8,000 pounds of cargo including roundworms to study muscle loss and the Spaceborne Computer 2, as well as an experiment to study the protein-based manufacturing of artificial retinas.<a class="footnote-ref" id="fnref:112" href="#fn:112">112</a></td></tr><tr><th scope="row" rowspan="2">15</th><td>August 10, 202122:01</td><td>Antares 230+</td><td>MARS, LP-0A</td><td>Cygnus (enhanced)<a href="/facts/Cygnus_NG-16/HdWpB8dR">CRS NG-16</a><a href="/facts/Ellison_Onizuka/jJECVekD">Ellison Onizuka</a></td><td>3,723 kg (8210 lbs)<a class="footnote-ref" id="fnref:113" href="#fn:113">113</a></td><td>LEO (ISS)</td><td>Northrop Grumman</td><td>NASA (CRS)</td><td>Success</td></tr><tr><td colspan="9"></td></tr><tr><th scope="row" rowspan="2">16</th><td>February 19, 202217:40</td><td>Antares 230+</td><td>MARS, LP-0A</td><td>Cygnus (enhanced)<a href="/facts/Cygnus_NG-17/uLNn7AzU">CRS NG-17</a><a href="/facts/Piers_Sellers/9gsXWTDj">Piers Sellers</a></td><td>3,800 kg (8,400 lb)<a class="footnote-ref" id="fnref:114" href="#fn:114">114</a></td><td>LEO (ISS)</td><td>Northrop Grumman</td><td>NASA (CRS)</td><td>Success</td></tr><tr><td colspan="9"></td></tr><tr><th scope="row" rowspan="2">17</th><td>November 7, 202210:32</td><td>Antares 230+</td><td>MARS, LP-0A</td><td>Cygnus (enhanced)<a href="/facts/Cygnus_NG-18/DndRMe9K">CRS NG-18</a><a href="/facts/Sally_Ride/fAAYVYj1">Sally Ride</a></td><td>3,652 kg (8,051 lb)<a class="footnote-ref" id="fnref:115" href="#fn:115">115</a></td><td>LEO (ISS)</td><td>Northrop Grumman</td><td>NASA (CRS)</td><td>Success</td></tr><tr><td colspan="9"></td></tr><tr><th scope="row" rowspan="2">18</th><td>August 2, 202300:31</td><td>Antares 230+</td><td>MARS, LP-0A</td><td>Cygnus (enhanced)<a href="/facts/Cygnus_NG-19/BcytlXhW">CRS NG-19</a><a href="/facts/Laurel_Clark/dq1EulUR">Laurel Clark</a></td><td>3,729 kg (8,221 lb)<a class="footnote-ref" id="fnref:116" href="#fn:116">116</a></td><td>LEO (ISS)</td><td>Northrop Grumman</td><td>NASA (CRS)</td><td>Success</td></tr><tr><td colspan="9">Final Antares 230+ launch.</td></tr></tbody></table>
Note: <a href="/facts/Cygnus_CRS_OA-4/HtLyNnDa">Cygnus CRS OA-4</a>, the first Enhanced Cygnus mission, and <a href="/facts/Cygnus_CRS_OA-6/xNGIoBdF">Cygnus OA-6</a> were propelled by <a href="/facts/Atlas_V/5SNgegyt">Atlas V</a> 401 launch vehicles while the new Antares 230 was in its final stages of development. <a href="/facts/Cygnus_CRS_OA-7/dPd7w0ge">Cygnus CRS OA-7</a> was also switched to an <a href="/facts/Atlas_V/5SNgegyt">Atlas V</a> 401 and launched on April 18, 2017
<h2 id="future-launches">Future launches</h2>
This section is transcluded from <a href="/facts/List_of_Antares_launches/G3lHnW9V">List of Antares launches</a>. (<a href="https://en.wikipedia.org/w/index.php?title=List_of_Antares_launches&action=edit">edit</a> | <a href="https://en.wikipedia.org/w/index.php?title=List_of_Antares_launches&action=history">history</a>)

<table><tbody><tr><th scope="col">Date / time (<a href="/facts/Coordinated_Universal_Time/2EnjfSyu">UTC</a>)</th><th scope="col">Rocket variant</th><th scope="col">Launch site</th><th scope="col">Payload</th><th scope="col">Orbit</th><th scope="col">Customer</th></tr><tr><td scope="row" rowspan="2">Q4 2025<a class="footnote-ref" id="fnref:117" href="#fn:117">117</a></td><td>Antares 330</td><td>MARS, LP-0A</td><td>Cygnus (Mission B)<a href="/facts/Cygnus_NG-23/8jFp6gs7">CRS NG-23</a></td><td>LEO (ISS)</td><td>NASA</td></tr><tr><td colspan="5">First flight of the Antares 330.</td></tr><tr><td scope="row" rowspan="2">2026<a class="footnote-ref" id="fnref:118" href="#fn:118">118</a></td><td>Antares 330</td><td>MARS, LP-0A</td><td>Cygnus (Mission B)CRS NG-24</td><td>LEO (ISS)</td><td>NASA</td></tr><tr><td colspan="5">Second flight of the Antares 330.</td></tr><tr><td scope="row" rowspan="2">2026<a class="footnote-ref" id="fnref:119" href="#fn:119">119</a></td><td>Antares 330</td><td>MARS, LP-0A</td><td>Cygnus (Mission B)CRS NG-25</td><td>LEO (ISS)</td><td>NASA</td></tr><tr><td colspan="5">Third flight of the Antares 330.</td></tr></tbody></table>
Note: <a href="/facts/Cygnus_NG-20/uvU8Mutq">Cygnus NG-20</a> and <a href="/facts/Cygnus_NG-21/x4MIV2Ds">Cygnus NG-21</a> were propelled by <a href="/facts/Falcon_9_Block_5/0QqsLwWb">Falcon 9 Block 5</a> launch vehicles while the new Antares 330 is in development. <a href="/facts/Cygnus_NG-22/8jFp6gs7">Cygnus NG-22</a> was damaged in transit and will not be launched.

<h2 id="launch-sequence">Launch sequence</h2>
The following table shows a typical launch sequence of Antares-100 series rockets, such as for launching a <a href="/facts/Cygnus_(spacecraft)/8jFp6gs7">Cygnus</a> spacecraft on a <a href="/facts/Commercial_Orbital_Transportation_Services/wYMHLjrk">cargo resupply mission</a> to the International Space Station.<a class="footnote-ref" id="fnref:120" href="#fn:120">120</a> The coast phase is required because the solid-fuel upper stage has a short burn time.<a class="footnote-ref" id="fnref:121" href="#fn:121">121</a>

<table><tbody><tr><th>Mission time</th><th>Event</th><th>Altitude</th></tr><tr><td>T− 03:50:00</td><td>Launch management call to stations</td><td></td></tr><tr><td>T− 03:05:00</td><td>Poll to initiate liquid oxygen loading system chilldown</td><td></td></tr><tr><td>T− 01:30:00</td><td>Poll for readiness to initiate propellant loading</td><td></td></tr><tr><td>T− 00:15:00</td><td><a href="/facts/Cygnus_(spacecraft)/8jFp6gs7">Cygnus</a>/payload switched to internal power</td><td></td></tr><tr><td>T− 00:12:00</td><td>Poll for final countdown and MES medium flow chilldown</td><td></td></tr><tr><td>T− 00:11:00</td><td>Transporter-Erector-Launcher (TEL) armed for rapid retract</td><td></td></tr><tr><td>T− 00:05:00</td><td>Antares avionics switched to internal power</td><td></td></tr><tr><td>T− 00:03:00</td><td>Auto-sequence start (terminal count)</td><td></td></tr><tr><td>T− 00:02:00</td><td>Pressurize propellant tanks</td><td></td></tr><tr><td>T− 00:00:00</td><td>Main engine ignition</td><td></td></tr><tr><td>T+ 00:00:02.1</td><td>Liftoff</td><td>0</td></tr><tr><td>T+ 00:03:55</td><td>Main engine cut-off (MECO)</td><td>102 km (63 mi)</td></tr><tr><td>T+ 00:04:01</td><td>Stage one separation</td><td>108 km (67 mi)</td></tr><tr><td>T+ 00:05:31</td><td>Fairing separation</td><td>168 km (104 mi)</td></tr><tr><td>T+ 00:05:36</td><td>Interstage separation</td><td>170 km (106 mi)</td></tr><tr><td>T+ 00:05:40</td><td>Stage two ignition</td><td>171 km (106 mi)</td></tr><tr><td>T+ 00:07:57</td><td>Stage two burnout</td><td>202 km (126 mi)</td></tr><tr><td>T+ 00:09:57</td><td>Payload separation</td><td>201 km (125 mi)</td></tr></tbody></table>
<h2 id="see-also">See also</h2>
<ul>
<li>Spaceflight portal</li></ul>
<ul><li><a href="/facts/Comparison_of_orbital_launchers_families/w5HG4Juq">Comparison of orbital launchers families</a></li>
<li><a href="/facts/Minotaur-C/XQDB2hca">Minotaur-C</a></li>
<li><a href="/facts/Falcon_9/mNck6vby">Falcon 9</a></li></ul>

<h2 id="external-links">External links</h2>

Wikimedia Commons has media related to Antares (rocket).

<ul><li><a href="https://www.northropgrumman.com/space/antares-rocket/">Official website</a></li></ul>

<h2 id="references">References</h2>

<ol>
<li id="fn:1">"Russian Rocket Engine Deliveries to the U.S. Evade Sanctions". The St. Petersburg Times (sptimes.ru). August 15, 2014. Archived from the original on August 18, 2014. Retrieved May 2, 2025. <a href="https://web.archive.org/web/20140818094312/http://sptimes.ru/index.php?action_id=2&story_id=40540" target="_blank">https://web.archive.org/web/20140818094312/http://sptimes.ru/index.php?action_id=2&story_id=40540</a> <a href="#fnref:1" class="footnote-back-ref">↩</a></li>
<li id="fn:2">Bergin, Chris (February 25, 2008). "none". Space News. p. 12. <a href="#fnref:2" class="footnote-back-ref">↩</a></li>
<li id="fn:3">Chris Bergin (December 23, 2008). "SpaceX and Orbital win huge CRS contract from NASA". nasaspaceflight.com. Retrieved February 22, 2015. <a href="https://www.nasaspaceflight.com/2008/12/spacex-and-orbital-win-huge-crs-contract-from-nasa/" target="_blank">https://www.nasaspaceflight.com/2008/12/spacex-and-orbital-win-huge-crs-contract-from-nasa/</a> <a href="#fnref:3" class="footnote-back-ref">↩</a></li>
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</ol>

Antares (rocket) open-in-new

Antares (rocket)