INSAT-4CR
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| Mission type | Communications |
|---|---|
| Operator | ISRO |
| COSPAR ID | 2007-037A |
| SATCAT № | 32050 |
| Website | http://www.isro.org/satellites/insat-4cr.aspx |
| Mission duration | 12 years (planned) |
| Spacecraft properties | |
| Bus | I-2K |
| Manufacturer | ISRO |
| Launch mass | 2,168 kilograms (4,780 lb) |
| Power | 3000 W |
| Start of mission | |
| Launch date | 2 September 2007, 12:51 UTC |
| Rocket | GSLV Mk.I F04 |
| Launch site | Satish Dhawan SLP |
| Orbital parameters | |
| Reference system | Geocentric |
| Regime | Geostationary |
| Longitude | 74° East |
| Perigee | 35,779 kilometres (22,232 mi)[1] |
| Apogee | 35,809 kilometres (22,251 mi)[1] |
| Inclination | 0 degrees[1] |
| Period | 1,436.1 minutes[1] minutes[1] |
| Transponders | |
| Band | 12 Ku band |
| Coverage area | India |
| TWTA power | 140 watts |
| EIRP | 51.5 decibel-watts |
INSAT-4CR is a communications satellite operated by ISRO as part of the Indian National Satellite System. Launched in September 2007, it replaced the INSAT-4C satellite which had been lost in a launch failure the previous year. The satellite is stationed in geostationary orbit at a longitude of 74 degrees east, and is expected to operate for ten years, however this may have been reduced by the underperformance of the Geosynchronous Satellite Launch Vehicle which placed it into orbit.
Spacecraft
INSAT-4CR was constructed by ISRO, and is based around the I-2K satellite bus.[2] A 2,168-kilogram (4,780 lb) spacecraft, it is equipped with twelve Ku band transponders operating at a frequency of 36 MHz, with 140 Watt travelling wave tube amplifiers. The satellite has an effective isotropic radiated power of 51.5 dBW. An additional Ku band signal is used as a beacon for tracking.
INSAT-4CR operates in a geostationary orbit at a longitude of 74 degrees east, providing communications to India.[3] Broadcasting capacity on INSAT-4CR is allocated to Airtel Digital TV and Sun Direct DTH. At launch, the satellite was carrying 1,218 kilograms (2,685 lb) of fuel,[2] for raising itself into geostationary orbit, and subsequently operateing there for a planned twelve years.[4] Increased expendature of fuel reaching geostationary orbit, due to launch underperformance, may have resulted in a loss of up to five years of operational life.[5]
Launch
INSAT-4CR was launched on 2 September 2007 by the fifth flight of the Geosynchronous Satellite Launch Vehicle, GSLV-F04. The launch occurred at 12:51 UTC on 2 September 2007.[6] The third stage of the carrier rocket underperformed, resulting in the satellite being placed into a lower than planned orbit.
As a result of the underperformance during its launch, INSAT-4CR had to expend manoeuvring and station keeping propellant to raise its orbit by more than had originally been planned. It was subsequently reported by Indian news agencies that ISRO had lost track of the satellite's orbit, and could not locate the spacecraft until NASA identified it several days later, however ISRO denied these claims.[5][7] As a result of these failures, the operational lifetime of the satellite was reportedly decreased by up to five years.[5]
References
- ↑ 1.0 1.1 1.2 1.3 1.4 Lua error in package.lua at line 80: module 'strict' not found.
- ↑ 2.0 2.1 Lua error in package.lua at line 80: module 'strict' not found.
- ↑ Lua error in package.lua at line 80: module 'strict' not found.
- ↑ Lua error in package.lua at line 80: module 'strict' not found.
- ↑ 5.0 5.1 5.2 Lua error in package.lua at line 80: module 'strict' not found.
- ↑ Lua error in package.lua at line 80: module 'strict' not found.
- ↑ Lua error in package.lua at line 80: module 'strict' not found.
