selected to provide 28 Block II (operational) Navstar GPS satellites. Development of the
satellites continued throughout Phase II.
Phase II for the User Segment was divided into two parts. In Phase IIA, starting in July 1979,
four contractors were selected to conduct performance analyses and preliminary design of UE. In
Phase IIB, starting in 1982, two of the four contractors were selected to continue UE
development. Phase IIB included design refinement, fabrication of prototypes, qualification
testing, and extensive field testing of the UE. The UE was tested at YPG and at sea. Testing at
sea was conducted by Naval Ocean Systems Center located in San Diego, California.
1.6.4 Phase III Production and Deployment (1986 to Present)
1.6.4.1 Space Segment (1986 to Present)
The Block II satellites were originally designed to be launched aboard the Space Transportation
System (Space Shuttle). Following an accident with the Space Shuttle Challenger in 1986, the
Block II satellite to launch vehicle interface was modified to enable launch aboard the Delta II
booster. The first Block II satellite was launched on 14 February 1989. The combined
constellation of Block I and Block II satellites achieved worldwide two dimensional positioning
capability in June 1991. Worldwide 3 D capability was achieved in 1993. The Initial Operational
Capability (IOC) was declared on 8 December 1993. A full 24 satellite constellation of Block II
satellites was achieved in April 1994. The military Full Operational Capability is planned for
1995. The remaining Block II satellites will be launched on demand. Table 1 2 is a summary of
the Block II launch dates and status.
In June of 1989 a contract was awarded for 20 GPS replenishment satellites, designated Block
IIR. The Block IIR satellites will have the capability to autonomously generate their own
navigation messages. The Block IIR production schedule may allow a first launch as early as
August 1996. In 1994, efforts were begun by the GPS JPO to procure additional Navstar
satellites to sustain the GPS satellite constellation past the year 2000. These satellites are
designated Block IIF (Follow On). The contract to provide the Block IIF satellites is planned for
November 1995. The planned production schedule supports a first launch in the year 2001.
In 1994 the GPS JPO also began studies for an Augmented GPS (AGPS). The AGPS concept is
to enhance the availability, accuracy and integrity of the GPS system using up to six geostationary
AGPS satellites. The satellites would broadcast integrity information and range corrections for all
GPS satellites via GPS like ranging signals.
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