Antares-110 (A-One) [NASA]
Antares-120 (Cygnus CRS-1)
Antares-130 (Cygnus CRS-3)
Antares-230 (Cygnus CRS-5)
Orbital has developed a medium-class launch vehicle, dubbed Antares (formerly Taurus II), to extend its family of small-class Pegasus, Taurus and Minotaur launchers. The Antares design adapts elements from these proven launch technologies along with hardware from one of the world's leading launch vehicle integrators to provide low-cost and reliable access to space for civil, commercial and military Delta II-class payloads.
The first stage structure is manufactured by ukrainian Yuzhnoe company and features two sub-cooled LOX and Kerosene fueled AJ26-62 (americanized Russian NK-33) engines of N1/L3 heritage, built in the early 1970ies. The stage structure is based on the Zenit launch vehicle. The second stage is a Castor-30, which is based on a shortened Castor-120 solid rocket motor. A Castor-30A second stage helps propel the first two Antares-110 rockets into orbit, then a higher-performing Castor-30B motor was used with the Antares-120 on the third and fourth flights in 2013. On the fifth flight, the stretched Castor-30XL upper stage was introduced on the Antares-130. The optional third stage called BTS (Bi-Propellant Third Stage, formerly ORK, Orbit Raising Kit) is based on the propulsion system of Orbital's Star-2 satellite bus. For high energy orbits a Star-48BV can be used as third stage.
An enhanced version called Antares-130 featuring a Castor-30XL upper stage will be used for later flights.
Antares is designed to achieve a 98% or greater launch reliability. It was developed, manufactured and launched using identical management approaches, engineering standards and production and test processes used in Orbital's other major launch vehicles.
The vehicle is launched from a new launch pad LA-0A at Wallops Island, where the former Conestoga launch pad was located.
The different variants are encoded by a three digit number:
1. digit = first stage (1 = AJ26-62 powered first stage, 2 = RD-181 powered first stage
2. digit = second stage (1 = Castor-30A, 2 = Castor-30B, 3 = Castor-30XL)
3. digit = third stage (0 = none, 1 = BTS, 2 = Star-48BV)
In the aftermath of the explosion of the first Antares-130, Orbital decided to discontinue the AJ26-62 powered series due to reliability issues of the engine and to speed up the introduction of the re-engined Antares-200 series, now planned for early 2016. The re-engined version will use two RD-181 engines. This series will be replaced by the Antares-300 series, which will use the RD-181 engines at full thrust and will likely have an optimized tank and will use standard LOX instead of sub-cooled LOX.
|Version||Stage 1||Stage 2||Stage 3|
|Antares-110 (ex Taurus-2 (1))||2 × AJ26-62 (NK-33)||Castor-30A||-|
|Antares-120 (ex Taurus-2 (2))||2 × AJ26-62 (NK-33)||Castor-30B||-|
|Antares-121 (ex Taurus-2 (2) BTS)||2 × AJ26-62 (NK-33)||Castor-30B||BTS / 3 × IHI BT-4|
|Antares-122||2 × AJ26-62 (NK-33)||Castor-30B||Star-48BV|
|Antares-130 (ex Taurus-2e)||2 × AJ26-62 (NK-33)||Castor-30XL||-|
|Antares-131 (ex Taurus-2e BTS)||2 × AJ26-62 (NK-33)||Castor-30XL||BTS / 3 × IHI BT-4|
|Antares-132 (ex Taurus-2h)||2 × AJ26-62 (NK-33)||Castor-30XL||Star-48BV|
|Antares-230||2 × RD-181||Castor-30XL||-|
|Antares-231||2 × RD-181||Castor-30XL||BTS / 3 × IHI BT-4|
|Antares-232||2 × RD-181||Castor-30XL||Star-48BV|
No.TNo Type Date LS Fai Payload
1 1 Antares-110 21.04.2013 WI LA-0A Cygnus Mass Simulator / Dove 1 / PhoneSat v1a / PhoneSat v1b / PhoneSat v2a 2 2 Antares-110 18.09.2013 WI LA-0A Cygnus D1 3 1 Antares-120 09.01.2014 WI LA-0A Cygnus CRS-1 / Flock-1 1, ..., 28↑ / ArduSat 2↑ / LituanicaSAT 1↑ / LitSat 1↑ / SkyCube↑ / UAPSat 1↑ 4 2 Antares-120 13.07.2014 WI LA-0A Cygnus CRS-2 / Flock-1b 1, ..., 28↑ / TechEdSat 4↑ / MicroMAS↑ / GEARRS 1↑ / Lambdasat↑ 5 1 Antares-130 28.10.2014 WI LA-0A F Cygnus CRS-3 / Flock-1d 1, ..., 26↑ / Arkyd 3↑ / RACE↑ / GOMX 2↑ 6 1 Antares-230 18.10.2016 WI LA-0A Cygnus CRS-5 / Lemur-2 14, ..., 17 planned launches 7 2 Antares-230 xx.12.2016 WI LA-0A Cygnus CRS-7 / Violet↑ / SUSat↑ / UNSW-EC0↑ / i-INSPIRE 2↑ / ZA-AeroSat↑ / nSIGHT 1↑ / QARMAN↑ / 14-BISat↑ / YUsend-QB50↑ / Ex-Alta 1↑ / BUSAT 1↑ / LilacSat 1↑ / NJUST 1↑ / Aoxiang 1↑ / SOMP 2↑ / QBITO↑ / Aalto 2↑ / X-CubeSat↑ / EntrySat↑ / IP2SAT↑ / SpaceCube↑ / DUTHSat↑ / UPSat↑ / Hoopoe↑ / ANUSAT 2↑ / LINK↑ / SNUSAT 1↑ / SNUSAT 1b↑ / GAMASAT 1↑ / RoBiSAT 1↑ / RoBiSAT 2↑ / SamSat-QB50↑ / qbee50-LTU-OC↑ / BeEagleSat↑ / HAVELSAT↑ / Phoenix↑ / PolyITAN-2-SAU↑ / QBUS 1↑ / QBUS 2↑ / QBUS 3↑ / QBUS 4↑ / IceCube↑ / HARP↑ / CSUNSat 1↑ / CXBN 2↑ / OPEN↑ 8 3 Antares-230 xx.xx.2017 WI LA-0A Cygnus CRS-8 9 4 Antares-230 xx.xx.2017 WI LA-0A Cygnus CRS-9 10 5 Antares-230 xx.xx.2017 WI LA-0A Cygnus CRS-10 11 6 Antares-230 xx.xx.2018 WI LA-0A Cygnus CRS-11 xx x Antares-230 xx.xx.20xx WI LA-0A Cygnus CRS-xx xx x Antares-230 xx.xx.20xx WI LA-0A Cygnus CRS-xx xx x Antares-230 xx.xx.20xx WI LA-0A Cygnus CRS-xx xx x Antares-230 xx.xx.20xx WI LA-0A Cygnus CRS-xx xx x Antares-230 xx.xx.20xx WI LA-0A Cygnus CRS-xx xx x Antares-230 xx.xx.20xx WI LA-0A Cygnus CRS-xx ↑ = deployed via ISS airlock Failures: 5: Rocket exploded ~ 6 seconds after launch Launch sites: WI = Mid-Atlantic Regional Spaceport (MARS), Wallops Island, Virginia, USA / LA-0A