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 | ? |