Atlas V 521
Launch vehicle · USA
Original archive entry. The text, images and links below are kept as they were written.
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.
More at: Atlas V 521.
Related
- 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
Chronology
2 events
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.- Rainbow 1 (Cablevision 1) - . Payload: A2100AX. Mass: 4,328 kg (9,541 lb). Nation: USA. Agency: Cablevision. Manufacturer: Lockheed. Class: Communications. Type: Civilian communications satellite. Spacecraft: AS 2100. USAF Sat Cat: 27852 . COSPAR: 2003-033A. Apogee: 35,795 km (22,241 mi). Perigee: 35,779 km (22,231 mi). Inclination: 0.10 deg. Period: 1,436.10 min. Delayed from May 8 As of 2007 Mar 10 located at 61.68W drifting at 0.011W degrees per day..
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.- AMC-16 (GE-16) - .
Payload: A2100AXS. Mass: 4,200 kg (9,200 lb). Nation: USA.
Agency: SES Americom.
Manufacturer: Lockheed.
Program: Americom.
Class: Communications.
Type: Civilian communications satellite. Spacecraft: AS 2100.
USAF Sat Cat: 28472 . COSPAR: 2004-048A. Apogee: 35,791 km (22,239 mi). Perigee: 35,781 km (22,233 mi). Inclination: 0.10 deg. Period: 1,436.10 min.
AMC-16, like AMC-15, was a hybrid Ku/Ka-band satellite built by Lockheed Martin and based on the A2100 spacecraft platform. The spacecraft was to become operational in early 2005 from 85º West with a 15 year design life. The satellite carried 24 x 36 MHz/140 W Ku-band transponders and 12 x 125MHz/75 W spot beams. Coverage included the continental United States, Alaska, and Hawaii. Launch was delayed from December 6 and 16. As of 2007 Mar 9 located at 118.75W drifting at 0.002W degrees per day.