1975-118A
The Flight 5 satellite was actually spacecraft 8 (or possibly 7), the first of the heavier Block II satellites with a mass of 1040 kg. The last Block 1 satellites, spacecrafts 5 and 6, were kept in storage and later upgraded. The enlarged IR arrays had 6000 pixels. Shortly after orbit insertion, a fuel line ruptured (detected by the impact warning sensor) and attitude control was lost but later recovered. The spacecraft remained in a drift orbit in which it saw some operational use.
| DSP 8 | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 1975 Dec 14 | 0515:00 | Launch by Titan IIIC | CC |
| 0517? | SRM sep | ||
| 0519? | Stage 1 sep | ||
| 0520? | Fairing sep | ||
| 0522? | Stage 2 MECO | 151 x 398 x 28.6 | |
| 0523? | Stage 2 sep | ||
| 0620? | Transtage MES-1 | ||
| 1145? | MES-2 | ||
| 1145? | MECO-2 | ||
| 1200? | Transtage sep | 1436.0 35671 x 35785 x 3.0 | |
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