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GSat 5P
GSAT 5P [ISRO]
GSAT-5P is being planned as replacement forINSAT-3E and will carry 24 normal C-Band and 12 extended C-Band transponders with India Coverage. The spacecraft will be positioned at 55° East longitude with a mission life of 12 years.
The spacecraft weighs 2330 kg and payload power requirement is 1700 W. Spacecraft configuration and equipment panel layouts are finalised. Payload subsystems and other subsystem packages are under advanced stage of realisation.
The satellite was lost, when the launch vehicle lost control about 53 sec after launch.
| Nation: | India |
|---|---|
| Type / Application: | Communication |
| Operator: | Insat |
| Contractors: | ISRO |
| Equipment: | 12 C-band transponders, 12 extended C-band transponders |
| Configuration: | I-2K (I-2000) Bus |
| Propulsion: | 440 Newton thrust liquid apogee motor |
| Power: | 2 solar arrays (2600 W) |
| Lifetime: | 14 years |
| Mass: | 2310 kg; 975 kg (dry) |
| Orbit: | GEO |
| Satellite | COSPAR | Date | LS | Launch Vehicle | Remarks | |
|---|---|---|---|---|---|---|
| GSat 5P | 2010-F04 | 25.12.2010 | Sr SLP | F | GSLV Mk.1(3) |
References:
- ISRO:GSAT-5P
Further GSat missions:
- GSat 1 [I-2K]
- GSat 2 [I-2K]
- GSat 3 (EduSat) [I-2K]
- GSat 4 (HealthSat) [I-2K]
- GSat 5 [I-2K]
- GSat 5P [I-2K]
- GSat 6, 6A [I-2K]
- GSat 7 [I-2K]
- GSat 7A [I-2K]
- GSat 8 [I-3K]
- GSat 9 (South Asian Satellite) [I-2K]
- GSat 10 [I-3K]
- GSat 11 [I-6K]
- GSat 12, 12R (CMS 01) [I-1K]
- GSat 14 [I-2K]
- GSat 15 [I-3K]
- GSat 16 [I-3K]
- GSat 17 [I-3K]
- GSat 18 [I-3K]
- GSat 19 [I-3K]
- GSat 20 (GSat N2, CMS 03) [I-4K]
- GSat 22 [I-3K]
- GSat 23 [I-3K]
- GSat 24 (GSat N1, CMS 02) [I-3K]
- GSat 29 [I-3K]
- GSat 30 [I-3K]
- GSat 31 [I-2K]
- GSat 32 [I-8K]
