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GPS Block IIR

GPS Block IIR

Satellites
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Basic Information
Name
GPS Block IIR
Designation
GPS Block IIR
Alternate Designation
GPS IIR-M (Series of eight improved satellites)
Equipment Type
Satellites
Manufacturer
Lockheed Martin
Date of Introduction
1996
Description

The GPS Block IIR is an improved version of GPS Block II spacecraft with an automated operation mode independent of the ground control segment. The spherical error probable was cut to 7 meters, the satellite features re-programmable micro-processors and civil/commercial signal was added. Lockheed-Martin Block IIR satellites were launched beginning in 1996 and continuing through 2004. On June 23, 2004, the US Air Force launched successfully the GPS IIR-12 spacecraft aboard a Delta II launch system joining a constellation of 28 operational GPS satellites. GPS IIR-12 is the 11th GPS IIR satellite put into orbit successfully. GPS IIR-13 was put into orbit November 6 2004 totaling 30 satellites on orbit. Lockheed-Martin is developing the GPS IIR-M upgrade that will incorporate two new military signals for enhanced accuracy and a second civil signal on a different frequency to eight existing GPS IIR spacecraft already built and held in storage. In addition, the modernized series will offer a modernized antenna panel that provides increased signal power to receivers on the ground, enhanced encryption and anti-jamming capabilities for the military. The first upgraded GPS IIR spacecraft, designated GPS IIR-M1 or GPS IIR-14 (M), was launched by a Delta II rocket on 25 September 2005 at Cape Canaveral Air Force Station, Florida. Lockheed Martin and the US Air Force cleared the GPS IIR-14 (M) delivering civilian and military signals for operational use on December 19, 2005. The GPS IIR-15(M) was launched successfully by a Delta II rocket on 25 September 2006 from Cape Canaveral Air Force Station, Florida.

Overview (Deagel)
Group Satellites
Status Active
Also Known As GPS IIR-M (Series of eight improved satellites)
Origin United States of America
Contractor Lockheed Martin
Initial Operational Capability (IOC) 1996
Total Production 21
Specifications (Deagel)
Dimensions — Height 1,900 millimeter
Dimensions — Length 1,930 millimeter
Dimensions — Width 1.5 meter
Mass — Weight 1,075 kilogram
Performance — Orbit 20,200 kilometer
Performance — Positioning Accuracy 7 meter
Time — Service Life 10 year
Variants
Variant 1 GPS Block I
Variant 2 GPS Block II
Variant 3 GPS Block IIR
Variant 4 GPS Block IIF
Variant 5 GPS Block III
Variant 6 GPS Block IIIF
Details
Country of Origin United States
Classification
Domain
Air & Air Defense
Equipment Status
Active
Dimensions
Length
1.93 m
Width
1.5 m
Height
1.9 m
Weight
1075 kg
Operators (1)
United States
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