Comstar 4 |
USA |
Spacecraft n°: |
USA satellite n°: |
Designation | 12309 / 81018A |
Launch date | 21 Feb 1981 |
Launch site | CC, LC-36A |
Launch vehicle | Atlas-SLV3D Centaur-D (AC-42) |
Mission | Communications |
Geostationary orbit | 76°W, inclined |
Prime contractor | Hughes |
Platform | HS-351 |
Mass at launch | 1516 kg |
Mass in orbit | 911 kg |
Dimension | 2.38 m diameter x 6.34 m height |
Stabilization | Spin stabilized (56 rpm) |
DC power | BOL:570 W |
Design lifetime | 10 years |
Main transponders | 24 |
Backup transponders | |
Power | Horizontal: 5 W (TWTA) Vertical: 5.5 W (TWTA) |
Bandwidth | 36 MHz |
Coverage | CONUS |
EIRP max | 33 dBW |
Polarization | linear H/V |
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