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Atlas V 521
Part of Atlas V
American orbital launch vehicle. Atlas V with 5-m diameter payload fairing, single engine Centaur upper stage, and two strap-on solid boosters. Payloads: 10,161 kg (22,401 lb) to sun synchronous orbit; 6,485 kg (14,297 lb) to geosynchronous transfer orbit.

Status: Active. First Launch: 2003-07-17. Last Launch: 2004-12-17. Number: 2 . Payload: 10,161 kg (22,401 lb). Thrust: 6,549.00 kN (1,472,273 lbf). Gross mass: 433,000 kg (954,000 lb). Height: 65.50 m (214.80 ft). Diameter: 3.81 m (12.49 ft). Span: 6.91 m (22.67 ft).


More at: Atlas V 521.

Family: orbital launch vehicle. Country: USA. Spacecraft: AS 2100. Projects: Americom. Launch Sites: Cape Canaveral, Cape Canaveral LC41. Stages: Atlas CCB, Aerojet SRB, Centaur V1. Agency: Martin.

2003 July 17 - . 23:45 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC41. Launch Pad: SLC41. LV Family: Atlas V. Launch Vehicle: Atlas V 521.
2004 December 17 - . 12:07 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC41. Launch Pad: SLC41. LV Family: Atlas V. Launch Vehicle: Atlas V 521.

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