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Atlas V 411

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Atlas V 411
Part of Atlas V Family
American orbital launch vehicle. Atlas V with 4-m diameter payload fairing, single engine Centaur upper stage, and one strap-on solid booster. Payloads: 8,763 kg (19,320 lb) to sun synchronous orbit; 6,075 kg (13,393 lb) to geosynchronous transfer orbit.

Status: Active. First Launch: 2006-04-20. Last Launch: 2011-04-15. Number: 3 . Payload: 8,763 kg (19,319 lb). Thrust: 5,188.00 kN (1,166,308 lbf). Gross mass: 386,800 kg (852,700 lb). Height: 59.10 m (193.80 ft). Diameter: 3.81 m (12.49 ft). Span: 5.36 m (17.58 ft).

Family: orbital launch vehicle. Country: USA. Spacecraft: Intruder, AS 2100, Jumpseat-2. Launch Vehicles: Raven. Projects: Astra. Launch Sites: Cape Canaveral, Vandenberg, Vandenberg SLC3E, Cape Canaveral LC41. Stages: Atlas CCB, Aerojet SRB, Centaur V1. Agency: Martin.



2006 April 20 - . 20:27 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC41. Launch Pad: SLC41. LV Family: Atlas V. Launch Vehicle: Atlas V 411.
  • Astra 1KR - . Payload: A2100AXS. Mass: 4,332 kg (9,550 lb). Nation: Luxembourg. Agency: SES. Manufacturer: Lockheed. Program: Astra. Class: Communications. Type: Civilian communications satellite. Spacecraft Bus: AS 2100. Spacecraft: AS 2100. USAF Sat Cat: 29055 . COSPAR: 2006-012A. Apogee: 35,696 km (22,180 mi). Perigee: 35,631 km (22,140 mi). Inclination: 0.1000 deg. Period: 1,429.80 min.

    The first Centaur upper stage burn placed the stack into a 167 km x 22442 km x 24.8 deg transfer orbit. After a second burn the Centaur released the satellite into a 6470 km x 36240 km x 23.8 deg orbit, from which it would use its own engine to achieve final geosynchronous orbit. As of 2007 Mar 10 located at 19.18E drifting at 0.022W degrees per day.


2008 March 13 - . 10:02 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg SLC3E. LV Family: Atlas V. Launch Vehicle: Atlas V 411.
  • USA 200 - . Payload: Raven 5 / NROL-28. Nation: USA. Agency: Martin. Class: Surveillance. Type: ELINT. Spacecraft Bus: Raven satellite. Spacecraft: Raven satellite. USAF Sat Cat: 32706 . COSPAR: 2008-010A. Apogee: 35,780 km (22,230 mi). Perigee: 1,112 km (690 mi). Inclination: 63.6000 deg. Period: 720.00 min.

    Classified National Reconnaisance Office satellite placed in a Molniya orbit; orbital parameters are estimated. Believed to be the second in a new series carrying combined signals intelligence and early warning payloads. Probable sensors included the SBIRS HEO-2 infrared missile early warning package and the NASA/Los Alamos TWINS-B magnetospheric research payload.


2011 April 15 - . 04:24 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg SLC3E. LV Family: Atlas V. Launch Vehicle: Atlas V 411.
  • USA 229 - . Payload: Intruder 9 / NROL-34. Mass: 3,250 kg (7,160 lb). Nation: USA. Class: Surveillance. Type: Naval signals intelligence satellite. Spacecraft Bus: Intruder. Spacecraft: Intruder. USAF Sat Cat: 37386 . COSPAR: 2011-014A. Apogee: 1,200 km (700 mi). Perigee: 1,010 km (620 mi). Inclination: 63.4000 deg. Period: 107.40 min. Probable naval ocean surveillance satellite cluster; normally operate in 1100 km circular orbits with 63 deg inclination and carry equipment to track ships and aircraft via their radio transmissions..
  • USA 229 P/L 2 - . Payload: Intruder 9 / NROL-34. Mass: 3,250 kg (7,160 lb). Nation: USA. Class: Surveillance. Type: Naval signals intelligence satellite. Spacecraft Bus: Intruder. Spacecraft: Intruder. USAF Sat Cat: 37391 . COSPAR: 2011-014B. Apogee: 1,200 km (700 mi). Perigee: 1,010 km (620 mi). Inclination: 63.4000 deg. Period: 107.40 min. Probable naval ocean surveillance satellite cluster; normally operate in 1100 km circular orbits with 63 deg inclination and carry equipment to track ships and aircraft via their radio transmissions..


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