 









|
|
Home | AMC-16
|
AMC-16, like AMC-15, is a hybrid Ku/Ka-band satellite built by Lockheed Martin and based on the A2100 spacecraft platform. Planned to be launched on an Atlas V launch vehicle from Cape Canaveral, the spacecraft will become operational in early 2005 from 85º West. |
Spacecraft design
|
|
Lockheed Martin A2100AX
|
|
|
|
Orbital location
|
|
85o W.L.
|
 |
|
|
Launch Date / Vehicle |
|
4Q 2004 / Atlas V |
 |
|
|
Design Life |
|
15 years |
|
|
|
Ku-band payload |
|
24 x 36 MHz |
 |
|
|
Amp type |
|
Linearized TWTA
140 watts |
 |
|
|
Amp Redundancy |
|
two groups of 18 for 12 |
 |
|
|
Receiver redundancy |
|
4 for 2 |
 |
|
|
Coverage |
|
CONUS, Alaska,Hawaii |
 |
|
|
Beacon |
|
11702.0 MHz (H)
12198.0 MHz (V) |
|
|
|
|
|
|
|
|
|
Ka-band payload |
|
12 spot beams @ 125MHz (3 x 39 MHz subchannels) |
Amp type |
|
LTWTA, 75 watts |
 |
|
|
Amp Redundancy |
|
two groups of 9 for 6 |
 |
|
|
Receiver redundancy |
|
two groups of 2 for 1
two groups of 7 for 5 |
 |
|
|
Coverage |
|
CONUS, Alaska,Hawaii |
 |
|
|
Beacon |
|
18582.0 MHz (RHCP) |
|
|
|
|
|
|
|
|
|
|
|
|
|