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Atlas V 401
Part of Atlas V Family
American orbital launch vehicle. Atlas V version with a 4-m diameter payload fairing, single engine Centaur upper stage, and no strap-on solid boosters. Payloads: 7,095 kg (15,642 lb) to sun synchronous orbit; 4,950 kg (10,910 lb) to geosynchronous transfer orbit.

Status: Active. First Launch: 2002-08-21. Last Launch: 2017-04-18. Number: 36 . Payload: 7,095 kg (15,641 lb). Thrust: 3,827.00 kN (860,343 lbf). Gross mass: 338,640 kg (746,570 lb). Height: 58.30 m (191.20 ft). Diameter: 3.81 m (12.49 ft). Span: 3.81 m (12.49 ft).


More at: Atlas V 401.

Family: orbital launch vehicle. Country: USA. Spacecraft: Astro-200, BCP-5000, Intruder, LRO, MAVEN, PAN, Quasar, RBSP, Eurostar 2000, HS 601, MicroSat-100, Spacebus 3000, AS 2100, DMSP Block 5D-3, FalconSat, SA-200, SDS-3, NOSS-3, Cubesat, Mars Reconnaissance Orbiter, Midstar, Orbital Express Astro, RS-300, STPSat, SSTL-150, SDO, GPS Block 2F. Projects: Eutelsat. Launch Sites: Cape Canaveral, Vandenberg, Vandenberg SLC3E, Cape Canaveral LC41, Cape Canaveral SLC41. Stages: Atlas CCB, Centaur V1. Agency: Martin.

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