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Antares·Orbital Sciences Corporation

Antares 230+

retired
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Specifications

Status
retired
Height
42.5 m
Diameter
3.9 m
Mass
286,000 kg
Stages
3
Thrust
3,844 kN
Payload to LEO
8,200 kg
First flight
2019-11-02
Total launches
8
Success / Fail
8 / 0

Antares known during early development as Taurus II, is an expendable launch system developed by Orbital Sciences Corporation (now part of Northrop Grumman Innovation Systems after Northrop Grumman acquired Orbital ATK) and the Yuzhnoye Design Bureau to launch the Cygnus spacecraft to the International Space Station as part of NASA's COTS and CRS programs. Able to launch payloads heavier than 5,000 kg (11,000 lb) into low-Earth orbit, Antares is the largest rocket operated by Orbital ATK. Antares launches from the Mid-Atlantic Regional Spaceport and made its inaugural flight on April 21, 2013.

Propulsion

First stage

2×RD-1811,860 kN
RP-1 / LOX · staged-combustion
NPO EnergomashIsp 333s (vac)since 2015

Payloads it launched

29 loaded
CYGNUS NG-19
LEO
CYGNUS NG-18
LEO
NACHOS-1
LEO
CYGNUS NG-17
LEO
CYGNUS NG-16
LEO
DHABISAT (MYSAT-2)
LEO
ORCA-7
LEO
GUNSMOKE-J 2
LEO
IT-SPINS
LEO
ORCA-6
LEO
CYGNUS NG-15
LEO
CYGNUS NG-14
LEO
CYGNUS NG-13
LEO
ULTP
LEO
EDGECUBE
LEO
HUSKYSAT-1 (HO-107)
LEO
SWAMPSAT-2
LEO
VPM
LEO
AEROCUBE 15B
LEO
CIRIS
LEO
OBJECT N
LEO
CYGNUS NG-12
LEO
MAKERSAT 1
LEO
AEROCUBE 14A
LEO
ORCA-8
LEO
AEROCUBE 14B
LEO
ORBITAL FACTORY 2 (OF-2)
LEO
MINICARB
LEO
AEROCUBE 15A
LEO