Atlas V 431 (original) (raw)
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Atlas V 431
American orbital launch vehicle. Atlas V with 4-m diameter payload fairing, single engine Centaur upper stage, and three strap-on solid boosters. Payloads: 11,547 kg (25,458 lb) to sun synchronous orbit; 7,800 kg (17,196 lb) to geosynchronous transfer orbit.
Status: Active. First Launch: 2005-03-11. Last Launch: 2016-12-18. Number: 3 . Payload: 11,547 kg (25,456 lb). Thrust: 7,910.00 kN (1,778,230 lbf). Gross mass: 482,500 kg (1,063,700 lb). Height: 59.10 m (193.80 ft). Diameter: 3.81 m (12.49 ft). Span: 6.91 m (22.67 ft).
More at: Atlas V 431.
Family: orbital launch vehicle. Country: USA. Spacecraft: FS-1300, Eurostar 3000. Launch Sites: Cape Canaveral, Cape Canaveral LC41. Stages: Atlas CCB, Aerojet SRB, Centaur V1. Agency: Martin, Inmarsat.
2005 March 11 - . 21:42 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC41. Launch Pad: SLC41. LV Family: Atlas V. Launch Vehicle: Atlas V 431.
- Inmarsat-4 F1 - . Payload: Inmarsat 4A / Eurostar 3000GM. Mass: 5,959 kg (13,137 lb). Nation: International. Agency: Inmarsat. Manufacturer: EADS Astrium. Program: Inmarsat. Class: Communications. Type: Civilian communications satellite. Spacecraft: Eurostar 3000. USAF Sat Cat: 28628 . COSPAR: 2005-009A. Apogee: 36,011 km (22,376 mi). Perigee: 35,562 km (22,097 mi). Inclination: 3.00 deg. Period: 1,436.10 min.
Heaviest single payload to geosynchronous transfer orbit to that date. Delayed from October 2004, February 27, March 10, 2005. The satellite was to provide L-band mobile communications and wideband data transmission for Inmarsat's global network. As of 2007 Mar 11 located at 63.82E drifting at 0.000E degrees per day.
2009 November 23 - . 06:55 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC41. Launch Pad: SLC41. LV Family: Atlas V. Launch Vehicle: Atlas V 431.
- Intelsat IS-14 - . Mass: 5,663 kg (12,484 lb). Nation: USA. Agency: Martin. Program: Intelsat. Class: Communications. Type: Civilian communications satellite. Spacecraft: FS-1300. USAF Sat Cat: 36097 . COSPAR: 2009-064A. Apogee: 35,800 km (22,200 mi). Perigee: 35,775 km (22,229 mi). Inclination: 0.00 deg. Period: 1,436.10 min.
Communications satellite to replace IS-1R at 24 deg W over the Atlantic. The Centaur AV-024 upper stage maneuvered and then released the satellite into a 6157 km x 39094 km x 22.5 deg geosynchronous transfer orbit at 08:53 GMT. IS-14 then used its own propulsion to reach its operational orbit. Mass 2517 kg unfuelled.
2016 December 18 - . 19:13 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC41. Launch Pad: Cape Canaveral SLC41. LV Family: Atlas V. Launch Vehicle: Atlas V 431.
- Echostar 19 - . Nation: USA. Class: Communications. Type: Communications satellite. Spacecraft: FS-1300. USAF Sat Cat: 41893 . COSPAR: 2016-079A. Apogee: 65,110 km (40,450 mi). Perigee: 164 km (101 mi). Inclination: 25.60 deg.
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