2001-003A
Progress M1 No 254 originally was to launch 2001 Jan 18. Launch was delayed when Mir lost power. Launch mas was 7082 kg. Fuel load was 2677 kg. It will dock at Kvant-1. The vehicle was used to deorbit the Mir complex.
| Progress M1-5 | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 2001 Jan 24 | 0428:42 | Launch by Soyuz-U | LC1 |
| T+1:59 St 1 sep | |||
| T+2:40 GO sep | |||
| T+4:47 St 2 sep | |||
| T+4:57 KhO sep | |||
| T+8:46 St 3 MECO | |||
| 0437:31 | T+8:49 Blok I sep | 193 x 242 x 51.6 | |
| 0821:51 | TCM1 59.2s 4m/s | ||
| 0858:05 | TCM2 114s 8m/s | ||
| 2001 Jan 25 | 0525:08 | TCM3 2m/s 28s | |
| 2001 Jan 26 | 0303:22 | TCM4 21m/s 308s | |
| 0349:41 | TCM5 7m/s 107s | ||
| 2001 Jan 27 | 0323:26 | TCM6 4m/s 11s | |
| 0407:30 | TCM7 1.6m/s 5s | ||
| 0533:31 | Docked with Mir/Kvant | ||
| 2001 Mar 23 | 0032:47 | Begin M1-5 burn 1 9m/s | |
| 0053:38 | M1-5 burn 1 cutoff | ||
| 0110 | 88.6 190 x 219 x 51.6 | ||
| 0201:11 | M1-5 burn 2 9.6m/s | ||
| 0224:25 | M1-5 burn 2 cutoff | 150 x 215 x 51.6 | |
| 0507:36 | Burn 3, SKD, 33m/s? | ||
| 0531 | Still burning | ||
| 0543 | Entry | ||
| 0550 | Breakup | ||
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