Antares 110 (original) (raw)

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Part of Antares LV

American orbital launch vehicle. Originally designated Taurus II. Pad-launched launch vehicle using Pegasus upper stages and a first stage combining a Ukrainian Zenit lower stage fitted with 30-year old surplus Russian N1 moon program rocket engines.

Status: Active. First Launch: 2013-04-21. Last Launch: 2013-09-18. Number: 2 .

2 stage vehicle consisting of 1 x Antares Stage 1 + 1 x Castor 30.

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Antares 110 American orbital launch vehicle. Originally designated Taurus II. Pad-launched launch vehicle using Pegasus upper stages and a first stage combining a Ukrainian Zenit lower stage fitted with 30-year old surplus Russian N1 moon program rocket engines.

Antares 120 Antares variant with a more powerful ATK Castor 30B second stage replacing the Castor 30 used on earlier flights.

Antares 130 Antares variant with a stretched ATK Castor 30XL second stage replacing the Castor 30B used on earlier flights.

Antares 230 American orbital launch vehicle. Pad-launched launch vehicle using Pegasus upper stages and a first stage combining a Ukrainian Zenit lower stage fitted with RD-181 lox/kerosene engines in place of NK-33 engines disastorously used in the earlier versions.

Country: USA. Spacecraft: Cygnus, Cubesat. Launch Sites: Wallops Island LA0A, Wallops Island LP0A.

2013 April 21 - . 21:00 GMT - . Launch Site: Wallops Island. Launch Complex: Wallops Island LP0A. LV Family: Antares LV. Launch Vehicle: Antares 110.

Cygnus Mass Simulator - . Mass: 4,000 kg (8,800 lb). Nation: USA. Agency: NASA. Manufacturer: OSC. Program: ISS. Class: Manned. Type: Manned logistics spacecraft. Spacecraft: Cygnus. Decay Date: 2013-04-27 . USAF Sat Cat: 39142 . COSPAR: 2013-016A. Apogee: 161 km (100 mi). Perigee: 153 km (95 mi). Inclination: 51.61 deg. Period: 87.63 min.
First launch of the Antares launch vehicle, combining surplus rocket engines from the Soviet N1 moon rocket program with US-built components. The mass simulator carried instrumentation to measure the launch vehicle environment in preparation for future launches of the Cygnus spacecraft designed to carry cargo to the International Space Station. It also released four cubesats into independent orbits.
Dove-1 - . Mass: 3.00 kg (6.60 lb). Nation: USA. Class: Technology. Type: Technology satellite. Spacecraft: Cubesat. Decay Date: 2013-04-27 . USAF Sat Cat: 39143 . COSPAR: 2013-016B. Apogee: 169 km (105 mi). Perigee: 160 km (90 mi). Inclination: 51.62 deg. Period: 87.78 min. 3U cubesat, a demonstration satellite for Cosmogia, designed to return on-board system health data and validate the design for future Dove satellites, which will carry remote sensing payloads..
Alexander - . Mass: 1.00 kg (2.20 lb). Nation: USA. Class: Technology. Type: Technology satellite. Spacecraft: Cubesat. Decay Date: 2013-04-27 . USAF Sat Cat: 39144 . COSPAR: 2013-016C. Apogee: 152 km (94 mi). Perigee: 134 km (83 mi). Inclination: 51.60 deg. Period: 87.35 min. 1U cubesat from NASA's Ames Research Center, designed to demonstrate use of a commercial Nexus S mobile phone as a spacecraft avionics/computer system, together with an S-band radio, solar panels, GPS receiver, magnetorquers and reaction wheels..
Bell - . Mass: 1.00 kg (2.20 lb). Nation: USA. Class: Technology. Type: Technology satellite. Spacecraft: Cubesat. Decay Date: 2013-05-10 . USAF Sat Cat: 39145 . COSPAR: 2013-016D. Apogee: 150 km (90 mi). Perigee: 144 km (89 mi). Inclination: 51.61 deg. Period: 87.42 min. 1U cubesat from NASA's Ames Research Center, designed to demonstrate use of a commercial Nexus One Android-based mobile phone as a spacecraft avionics/computer system..
Graham - . Mass: 1.00 kg (2.20 lb). Nation: USA. Class: Technology. Type: Technology satellite. Spacecraft: Cubesat. Decay Date: 2013-04-26 . USAF Sat Cat: 39146 . COSPAR: 2013-016E. Apogee: 175 km (108 mi). Perigee: 161 km (100 mi). Inclination: 51.62 deg. Period: 87.85 min. 1U cubesat from NASA's Ames Research Center, designed to demonstrate use of a commercial Nexus One Android-based mobile phone as a spacecraft avionics/computer system..

2013 September 18 - . 14:58 GMT - . Launch Site: Wallops Island. Launch Complex: Wallops Island LA0A. LV Family: Antares LV. Launch Vehicle: Antares 110.

SS G David Low - . Payload: Cygnus OD-1. Mass: 4,127 kg (9,098 lb). Nation: USA. Agency: NASA. Manufacturer: OSC. Program: ISS. Class: Manned. Type: Manned logistics spacecraft. Spacecraft: Cygnus. Duration: 35.00 days. Decay Date: 2013-10-23 . USAF Sat Cat: 39258 . COSPAR: 2013-051A. Apogee: 414 km (257 mi). Perigee: 411 km (255 mi). Inclination: 51.65 deg. Period: 92.81 min.
First Orbital Sciences Cygnus ISS resupply spacecraft. Named SS G. David Low after the late astronaut, son of the former NASA administrator, and Orbital employee. The Cygnus consisted of a pressurized cargo module (PCM) built by Thales Alenia in Torino, and a service module (SM) built by Orbital/Dulles. The craft carried 700 kg of cargo. Intiial orbit was 261 km x 277 km x 51.6 deg; at 20:07 GMT this was raised to 274 km x 384 km. On 22 September the first attempt at rendezvous with the ISS was cancelled due to a software problem in the GPS navigation system; Cygnus passed ISS at a distance of 4 km at 08:45 GMT. On 29 September Cygnus completed its rendezvous with ISS, reaching a 250 m hold point at 09:08 GMT. The SSRMS arm captured Cygnus at 11:00 GMT, and after berthing to the Harmony module of the ISS he astronauts began unloading the ship's cargo. Cygnus unberthed from Harmony at 10:04 GMT on 22 October and was released into a 415 x 419 km orbit by the SSRMS at 11:31 GMT. On 23 October Cygnus conducted its retrofire burn at 17:41 GMT, and burnt up at 18:16 GMT over the South Pacific.

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