Intelsat 14: Difference between revisions
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Revision as of 07:53, 14 November 2009
 | This article needs additional citations for verification. (September 2007) |
| Spacecraft Design | Space Systems Loral |
|---|---|
| Orbital location | 45° West (0°N 45°W / 0°N 45°W) |
| Launch Date | 2009 |
| Vehicle | LS-1300 |
| Design Life | 15 years |
| Amplifier type | TWTA, 50 watts |
|---|---|
| Amplifier Redundancy: | 2 groups of 16 for 12
2 groups of 10 for 8 |
| Receiver redundancy: | 4 for 2 |
| Coverage: | Americas, Europe, Africa |
| C band Beacon | 3704.0 MHz Horizontal Polarization(H) |
| C band Beacon | 3705.0 MHz Vertical Polarization (V) |
| Amp type | TWTA, 120 watts |
|---|---|
| Amp Redundancy: | 2 groups of 14 for 11 |
| Receiver redundancy: | 4 for 2 |
| Coverage: | Americas, Europe, Africa |
| Ku band Beacon | 11694.0 MHz (V) |
| Ku band Beacon | 11695.0 MHz (H) |
Intelsat 14 is a future communications satellite owned by Intelsat planned to be located at 45° W longitude, serving the Americas market. Intelsat 14 is intended to replace Intelsat 1R which is nearing the end of its design life. It is currently being built by Space Systems Loral, as part of its LS-1300 line.
The clients for Intelsat 14 are expected to include the current clients for Intelsat 1R.
It carries the IRIS (Internet Router in Space) demonstration.[1]
References
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