1972-097A
Nimbus E was the first Nimbus satellite to be launched on a Delta. The Delta model 0900 launch vehicle ignited at 0756 on 1972 Dec 11; 35 seconds later the solid motors separated. Stage 1 separation occurred at T+3 min 48 sec, followed by a 3 min 52 sec Delta stage burn into transfer orbit, achieved at 0805 UT. At 0853 the Delta stage re-ignited to circularize the orbit, and separated from the payload at 0857. Nimbus E was now Nimbus 5, in a 1089 x 1102 km x 100.0 deg orbit. The Delta stage made two test burns and ended up in a more eccentric 1105 x 1528 km orbit. Nimbus 5 carried on sending back data until 1983 Apr 1.
| Nimbus 5 | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 1972 Dec 11 | 0756:00 | Launch by Delta 0900 | V |
| SRM sep | |||
| T+3:53 MECO | |||
| T+3:48? St 1 sep | |||
| T+4m? SES-1 5:12 | |||
| 0805? | SECO-1 | 180? x 1100? x 99 | |
| 0853 | T+57:05 SES-2 12s | ||
| 0853 | SECO-2 | ||
| 0857 | St 2 sep | 106.87 1062 x 1101 x 99.9 | |
| 0912? | SES-3 experimental | ||
| 0912? | SECO-3 | ||
| 0927? | SES-4 experimental | ||
| 0927? | SECO-4 | 1102 x 1519 x 99.8 (Delta) | |
| 1972 Dec 11 | 106.87 1062 x 1101 x 99.9 | ||
| 1983 Apr 1 | End of ops | ||
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