2003-008A
A-3 will be launched in 2003 to IOR. B-6 remains.
At this point the DSCS III program was run by LMSS/Sunnyvale and managed by AFSMC.
Launch by Delta IVM (no solids) with RL10B-2 second stage and 11.7m fairing from Cape Canaveral SLC37B. Launch mass 2732 kg including 1488? kg IABS. Power 1.7kW BOL. Target orbit 235 x 35551 km x 25.5 deg. The IABS stage was incorrectly registered with the UN in a transfer orbit. Some debris objects were probably associated with the Delta 4 second stage, perhaps in its transfer orbit burn.
| DSCS III A3 | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 2003 Mar 11 | 0059:00 | Launch by Delta IVM | CC SLC37B |
| T+4:19 MECO | |||
| T+4:30 St 1 sep | |||
| T+4:44 SES-1 579s 167 km | -5000? x 200? x 29? | ||
| T+4:55 Fairing sep 179 km | |||
| 0113:23 | T+14:23 SECO-1 | 186 x 401 x 29.20 | |
| 0125:03 | T+26:03 SES-2 248s | ||
| 0129:11 | T+30:11 SECO-2 | 233 x 35787 x 25.50 | |
| 0141:01 | T+42:01 St 2 sep | 234 x 35571 x 25.5 (UN) | |
| T+5:47:13 First asc. node | |||
| 2003 Mar 13? | 5th apo IABS burn 1 hr | ||
| T+4d 1 min trim burn | |||
| Despun | |||
| 2003 Mar 15? | IABS sep | ||
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