2000-034A
The HS-601 TDRS-H was the first of the new series TDRS, carrying S, Ku and Ka-band but omitting the C-band payload of the earlier models. Size is 21.0m span across solar panels, 13 m across antennas. Stowed 8.4m x 3.4m. Mass is 3180 kg launch, 1777 kg BOL. Will test at 150W and move to 171W for TDRS-West duties. The dish antennas provide single access S, Ku and Ka band capability; a phased array antenna supplies S-band multiple access.
In mid-2001 it was revealed that the phased-array antenna had been disappointing in checkout, and did not meet the spec performance. TDRS H was finally accepted by NASA-GSFC in Aug 2001.
| TDRS H | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 2000 Jun 30 | 1256 | Launch by Atlas 2A AC-139 | CC SLC36A |
| T+2:45 BECO | |||
| T+2:48 Booster sep | |||
| T+3:37 Fairing sep | |||
| T+4:35 SECO | |||
| T+4:37 Atlas sep | |||
| T+4:53 MES-1 | |||
| T+6:00 156 km 3.93 km/s | |||
| 1305 | T+9:46 MECO-1 | 167 x 577 x 28.3 | |
| 1321 | T+24:48 MES-2 | ||
| 1322 | T+26:08 MECO-2 | ||
| 1326 | T+29:55 Centaur sep | ||
| 1751 | Antenna deploy | 480.66 230 x 27665 x 27.1 | |
| 2000 Jul 3 | 2130? | LAM-1 | 638.04 389 x 35954 x 26.9 |
| 2000 Jul 4 | 1330? | LAM-2 | 752.16 6066 x 35971 x 17.4 |
| 2000 Jul 5 | 1700? | LAM-3 | 20307 x 35922 x 9? |
| 2000 Jul 7 | 1400s | LAM-3 | 1247.91 28061 x 35973 x 8.2 |
| 2000 Jul 8 | 1100s | LAM-4 | 1407.60 34396 x 36057 x 7.6 |
| 2000 Jul 9 | 0700s | Trim burn | |
| 2000 Jul 18 | 1435.88 35617 x 35947 x 7.0 GEO 150.3W | ||
| 2000 Oct 15 | 1436.04 35646 x 35924 x 6.9 GEO 150.4W | ||
| 2001 Dec 13 | 1436.03 35713 x 35856 x 5.9 GEO 150.4W | ||
| 2002 Jan 3 | Relocating from 150W | ||
| 2002 Jan 22 | Move in at 171W | ||
| 2002 Mar 22 | 1436.13 35773 x 35800 x 5.6 GEO 170.7W | ||
| 2004 Jan 2 | 1436.22 35775 x 35802 x 4.0 GEO 171.1W | ||
| 2004 May | Move to 174.5W | ||
| 2004 May 12 | 1436.06 35768 x 35803 x 3.7 GEO 174.5W | ||
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