
IRNSS [ISRO]
The Indian Government has approved in May 2006, a project to implement an Indian Regional Navigation Satellite System (IRNSS) in the next six to seven years. It will consist of a constellation of seven satellites and a large ground segment. Three of the seven satellites in IRNSS constellation will be placed in Geostationary Earth Orbit and four in Geosynchronous Orbits inclined at 29° to the equatorial plane. All the seven satellites will have continuous radio visibility with Indian control stations.
Each satellite has two payloads: a navigation payload and CDMA ranging payload in addition with a laser retro-reflector. The payload generates navigation signals at L5 and S-band. The design of the payload makes the IRNSS system inter-operable and compatible with GPS and Galileo.
| Nation: | India |
|---|---|
| Type / Application: | Navigation |
| Operator: | ISRO |
| Contractors: | ISRO |
| Equipment: | |
| Configuration: | I-1K (I-1000) Bus |
| Propulsion: | LAM engine |
| Power: | 2 deployable solar arrays, batteries |
| Lifetime: | |
| Mass: | 1300 kg |
| Orbit: | 3 in GEO, 4 in 29°-inclined GEO |
| Satellite | Date | LS | Launch Vehicle | Remarks | |
|---|---|---|---|---|---|
| IRNSS 1A | 2013 | Sr FLP | PSLV-HP | ||
| IRNSS 1B | 2013 | Sr | PSLV-HP | ||
| IRNSS 1C | 2014 | Sr | PSLV-HP | ||
| IRNSS 1D | 2014 | Sr | PSLV-HP | ||
| IRNSS 1E | 2015 | Sr | PSLV-HP | ||
| IRNSS 1F | 2015 | Sr | PSLV-HP | ||
| IRNSS 1G | 2015 | Sr | PSLV-HP |