GPS-2F (Navstar-2F)

 

GPS-2F [Boeing]

GPS-2F (Global Positioning System) or Navstar-2F (Navigation System using Timing And Ranging) satellites are the fourth evolution stage of the second generation of the GPS GPS satellites. Improvements included an extended design life of 12 years, faster processors with more memory, and a new civil signal on a third frequency. The first Block-IIF satellite is scheduled to launch in 2006

Boeing was contracted with options for up to 33 Block-IIF satellites in 1996, but in 2001 the contract was reduced 12 Block-IIF satellites. In July 2006, satellites 10, 11 and 12 were contracted.

The GPS-2F satellites do not need to carry an apogee kick motor, in contrast to the earlier generations, as the launch vehicles provide direct insertion into the GPS orbit. Originally the Delta-4M version was to be used for the Delta launches, but a mass growth of the satellites required a switch to the more powerful Delta-4M+(4,2) version. For Atlas launches, the Atlas-5(401) version is used.

Nation: USA
Type / Application: Navigation
Operator: USAF
Contractors: Boeing
Equipment: ?
Configuration: 3-Axis stabilized
Propulsion: ?
Power: 2 deployable solar arrays, batteries
Lifetime: 15 years
Mass: 1630 kg
Orbit: 20200 km × 20200 km, 55.0°
Satellite Date LS Launch Vehicle Remarks
GPS-2F 1 (Navstar 62, USA 213) 28.05.2010 CC SLC-37B Delta-4M+(4,2)
GPS-2F 2 (Navstar 63, USA 232) 16.07.2011 CC SLC-37B Delta-4M+(4,2)
GPS-2F 3 (Navstar xx) 2012 CC SLC-37B Delta-4M+(4,2)
GPS-2F 4 (Navstar xx) CC SLC-41 Atlas-5(401)
GPS-2F 5 (Navstar xx) CC SLC-41 Atlas-5(401)
GPS-2F 6 (Navstar xx) CC SLC-41 Atlas-5(401)
GPS-2F 7 (Navstar xx) CC SLC-41 Atlas-5(401)
GPS-2F 8 (Navstar xx) CC SLC-41 Atlas-5(401)
GPS-2F 9 (Navstar xx) CC SLC-37B Delta-4M+(4,2)
GPS-2F 10 (Navstar xx) CC SLC-37B Delta-4M+(4,2)
GPS-2F 11 (Navstar xx) CC Atlas-5(401) or Delta-4M+(4,2)
GPS-2F 12 (Navstar xx) CC Atlas-5(401) or Delta-4M+(4,2)