2015-019A
The satellite was also called Beidou I-1S. The first Beidou new-generation satellite flew on a new launch vehicle variant, a CZ-3C with a Yuanzheng-1 (Expedition) upper stage similar to Russia's Fregat. YZ-1 was about 3590 kg full 2075 kg at end of life, according to estimates in Novosti Kosmonavtiki.
| BDW17 | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 2015 Mar 30 | 1352 | Launch by CZ-3C | XSC |
| T+2:25 St 1 MECO | |||
| T+2:26 St 1 sep | |||
| T+4:19 Fairing sep | |||
| T+5:28 St 2 MECO | |||
| T+5:33 St 2 VECO | |||
| T+5:34 St 2 sep, St 3 MES | |||
| 1402 | T+10:51 MECO-1 | ||
| 1414 | T+22:03 MES2 | ||
| 1416 | T+24:35 MECO2 | ||
| 1418 | T+26:15? St 3 Sep | 438.83 194 x 25307 x 54.9 | |
| 1418? | YZ-1 burn 1 | ||
| YZ-1 cutoff | |||
| 1930? | YZ-1 burn 2 | ||
| YZ-1 cutoff | |||
| 1934 | T+5:42 Beidou sep | 1461.8 35797 x 36781 x 55.0 | |
| 2010? | YZ-1 burn 3 -80m/s? | ||
| YZ-1 cutoff | 27000? x 36000? | ||
| 2015 Mar 31 | 0630? | YZ-1 burn 4 | |
| YZ-1 cutoff | 5175.3 27018 x 157986 x 41.2 | ||
| 2015 Apr 1 | 0823? | YZ-1 pass EL1:4 | |
| 2015 Apr 2 | 1461.84 35797 x 36781 x 55.0 | ||
| 2015 Apr 28 | braking | 1435.74 35605 x 35953 x 55.0 | |
| 2015 Jun 5 | 1435.89 35598 x 35966 x 55.0 GSO 84-112E | ||
| 2015 Jun 17 | 1435.93 35597 x 35968 x 54.9 | ||
No comments:
Post a Comment