1989-026A
The third of the SDIO Delta missions was Delta Star, again with an APL payload, this time separate from the McDonnell Douglas Delta second stage. McDonnell Douglas made the spacecraft bus. The hydrazine propulsion system was adapted from Block II GPS. The first target was its own second stage which made a deorbit burn. The reentry was reported to be at 2336 UTC over the Indian Ocean; this is not consistent with the orbit data, and must mean that the burn was at 2336 UTC over N America, but the entry was at around 0015 UTC over the Indian Ocean. The Black Star sounding rocket missions were also observed.
| Delta Star | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 1989 Mar 24 | 2150:49 | Launch by Delta 3920 | CC LC17 |
| 2154:29 | Thor MECO (T+3:40) | ||
| 2154:43 | Delta burn (T+3:54) | ||
| 2201:02 | Delta SECO (T+10:13) | 182? x 524? x 36.4? | |
| 2230? | Delta SES-2 4s | ||
| 2230? | Delta SECO-2 | 482 x 503 x 47.7 | |
| 2235? | Delta sep | ||
| 2237? | Delta deorbit burn 9s | ||
| 2310? | Delta depletion burn 4s | ||
| 2336 | T+1:45:55 Delta reentry burn | ||
| 1989 Mar 25 | 0015? | Delta reentry | |
| 1989 Mar 29 | 94.47 482 x 503 x 47.7 | ||
| 1989 Apr 2 | 94.57 485 x 512 x 47.7 | ||
| 1989 Apr 25 | 94.46 483 x 502 x 47.7 | ||
| 1989 Apr 26 | 94.51 488 x 502 x 47.7 | ||
| 1989 May 3 | 94.50 488 x 501 x 47.7 | ||
| 1989 May 4 | 94.54 491 x 502 x 47.7 | ||
| 1989 May 7 | 94.60 496 x 504 x 47.7 | ||
| 1989 May 9 | 94.63 497 x 505 x 47.7 | ||
| 1989 May 24 | 94.60 488 x 511 x 47.7 | ||
| 1989 May 25 | 94.79 497 x 519 x 47.7 | ||
| 1989 May 27 | 94.76 497 x 517 x 47.7 | ||
| 1989 Jun 2 | 94.43 471 x 511 x 47.7 | ||
| 1989 Jun 10 | 94.40 471 x 509 x 47.7 | ||
| 1989 Jun 16 | 94.53 477 x 515 x47.7 | ||
| 1989 Jun 21 | 94.52 476 x 514 x 47.7 | ||
| 1989 Jun 24 | 94.47 475 x 509 x 47.7 | ||
| 1989 Jul 8 | 94.44 474 x 508 x 47.7 | ||
| 1989 Jul 21 | 94.51 480 x 509 x 47.7 | ||
| 1989 Jul 30 | 94.49 479 x 507 x 47.7 | ||
| 1989 Aug 16 | 94.53 483 x 508 x 47.7 | ||
| 1989 Aug 25 | 94.40 481 x 497 x 47.7 | ||
| 1989 Aug 28 | 94.86 484 x 539 x 47.7 | ||
| 1989 Sep 1 | 94.85 483 x 538 x 47.7 | ||
| 1989 Oct 15 | 94.48 483 x 503 x 47.7 | ||
| 1989 Dec | orbit lowering burns | ||
| 1989 Dec 27 | end of ops | ||
| 1992 Jun 23 | Reentered | ||
Payload:
- Hughes LWIR camera
- GE IR imager
- Materials experiment
- Laser/radar
- JPL 4-channel UV imager
- AFA video camera
- APL visible imagers (2)
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