DSCS 3-05 |
USA |
Spacecraft n°: |
US spacecraft n°: |
Designation | 21873 / 92006A |
Launch date | 11 Feb 1992 |
Launch site | CC, LC-36B |
Launch vehicle | Atlas-2 (AC-101) |
Mission | Military:Telecommunications |
Geostationary orbit on: | |
Perigee / Apogee | km |
Eccentricity | |
Inclination | deg |
Period | min |
Prime contractor | Lockheed Martin (former GE Astro Space) |
Platform | |
Operator | |
Mass at launch | 2615 kg |
Mass in orbit | 1170 kg |
Basic shape | |
Dimension (m) | 2.07 x 1.93 x 1.96m (LxWxD) |
Solar array | 11.4m |
Stabilization | 3 axis |
DC power | BOL: 1240 W EOL; 837 W three 35 AH NiCd batteries |
Telemetry | S- and X-band |
Beacon | 7600.0 and 7604.7 MHz |
Design lifetime | 10 yrs |
Main transponders | 6 |
Backup | two 40 W and two 10 W amplifiers |
Power |
channels
1 & 2: 40 W (TWTA) channels 3 to 6: 10 W (SSPA) |
Coverage and EIRP max |
2
Global beams: 29 dBW 2 Spot beams: 34 dBW Gimballed dish: 44 dBW |
Channel | Bandwidth (MHz) | Frequency |
1 | 50 | ? |
2 | 75 | ? |
3 | 85 | ? |
4 | 85 | ? |
5 | 60 | ? |
6 | 50 | ? |