Navstar-2R [Lockheed] |
Navstar-2R (Navigation System using Timing And Ranging) or GPS-2R are the third evolution stage of the second generation of the Navstar GPS satellites
The GPS-IIR replenishment satellites are produced by General Electric Astrospace (later Martin Marietta and Lockheed Missiles & Space) under a contract issued in 1989, which included 21 satellites based on the commercial AS-4000 bus. These provided improved navigation accuracy and longer autonomous satellite operation than earlier model GPS satellites. The satellites were three-axis stabilized and operated at downlink frequencies of 1572.42 MHz and 1227.6 MHz (L-Band) and 2227.5 MHz (S-Band). Lockheed was responsible for launch and flight operations support of the GPS IIR through 2006.
Block IIR satellites provided dramatic improvements over previous blocks. They could determine their own position by performing inter-satellite ranging with other IIR vehicles. They also had reprogramable satellite processors enabling problem fixes and upgrades in flight, increased satellite autonomy, and radiation hardness.
Additionally, the Block IIR could be launched into any of the required GPS orbits at any time, assuming a 60-day advanced notice,
and required many fewer ground contacts to maintain the constellation. All of these
improvements result in increased accuracy for GPS users
and a cost 33 percent less per satellite than the previous generation of Block IIA satellites. Up to 12 Block IIR satellites were to be
modified to use the new military M-code on both the L1 and L2 channel as well as the more
robust civil signal L2C on the L2 channel. The M-code signal was to enable GPS operations in a higher jamming environment and reduce
vulnerability of military GPS-based systems. The first modified Block IIR (or IIR-M) is planned for launch 2004.
| Nation: | USA |
|---|---|
| Type / Application: | Navigation |
| Operator: | USAF |
| Contractors: | Lockheed Martin |
| Equipment: | ? |
| Configuration: | AS-4000 |
| Propulsion: | Star-37FM |
| Lifetime: | 10 years |
| Mass: | 2032 kg |
| Orbit: | 20200 km x 20200 km, 55.0° |
| Satellite | Date | LS | Launcher | Remarks: | |
|---|---|---|---|---|---|
| Navstar-2R 1 (GPS 42) | 16.01.1997 | CC LC-17A | F | Delta-7925 | |
| Navstar-2R 2 (GPS 43, USA 132) | 23.07.1997 | CC LC-17A | Delta-7925 | ||
| Navstar-2R 3 (GPS 46, USA 145) | 07.10.1999 | CC SLC-17A | Delta-7925 | ||
| Navstar-2R 4 (GPS 51, USA 150) | 11.05.2000 | CC SLC-17A | Delta-7925 | ||
| Navstar-2R 5 (GPS 44, USA 151) | 16.07.2000 | CC SLC-17A | Delta-7925 | ||
| Navstar-2R 6 (GPS 41, USA 154) | 10.11.2000 | CC SLC-17A | Delta-7925 | ||
| Navstar-2R 7 (GPS 54, USA 156) | 30.01.2001 | CC SLC-17A | Delta-7925 | ||
| Navstar-2R 8 (GPS 56, USA 166) | 29.01.2003 | CC SLC-17B | Delta-7925 | with XSS 10 | |
| Navstar-2R 9 (GPS 45, USA 168) | 31.03.2003 | CC SLC-17A | Delta-7925 | ||
| Navstar-2R 10 (GPS 47, USA 175) | 21.12.2003 | CC SLC-17A | Delta-7925 | ||
| Navstar-2R 11 (GPS 59, USA 177) | 20.03.2004 | CC SLC-17B | Delta-7925 | ||
| Navstar-2R 12 (GPS 60, USA 178) | 23.06.2004 | CC SLC-17B | Delta-7925 | ||
| Navstar-2R 13 (GPS 61, USA 180) | 06.11.2004 | CC SLC-17B | Delta-7925 | ||
| Navstar-2R 14 (GPS 53) | converted | -> Navstar-2RM 1 | |||
| Navstar-2R 15 (GPS 52) | converted | -> Navstar-2RM 2 | |||
| Navstar-2R 16 (GPS 58) | converted | -> Navstar-2RM 3 | |||
| Navstar-2R 17 (GPS 55) | converted | -> Navstar-2RM 4 | |||
| Navstar-2R 18 (GPS 57) | converted | -> Navstar-2RM 5 | |||
| Navstar-2R 19 (GPS 49) | converted | -> Navstar-2RM 6 | |||
| Navstar-2R 20 (GPS 48) | converted | -> Navstar-2RM 7 | |||
| Navstar-2R 21 (GPS 50) | converted | -> Navstar-2RM 8 |
| Further Navstar missions: |
Last update: 27.09.2009
Contact: gunter.krebs@skyrocket.de
© Gunter Dirk Krebs