1988-059A
The second Fobos, 1F No. 102, was launched on 1988 Jul 12 using the same profile as 1F No. 101.
The spacecraft would have deployed landers on the surface of Phobos. As well as the long-lived lander, Fobos-2 carried a 'hopper' lander.
On Mar 21 Fobos-2 entered a quasisynchronous orbit relative to Phobos, ranging between 200 and 600 km from the moon.
The spacecraft failed for unknown reasons on 1989 Mar 27. The failure review determined that most likely the problem was with the on-board computer, although meteorite hits or an electrical charging problem were not ruled out. The probe lost orientation and then electrical power. The plan had been for Phobos rendezvous and lander separation on 1989 Apr 4-5.
| Fobos-2 | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 1988 Jul 12 | 1701:43 | Launch by Proton-K | KB |
| 1711? | Stage 3 MECO | ||
| 1711? | Stage 3 sep | ||
| 1988 Jul 12 | 1717:30? | Blok-D-2 burn 1 | |
| 1719:04? | Blok-D-2 cutoff | 88.07 161 x 197 x 51.51 | |
| 1810? | SOZ units sep | ||
| 1810? | Blok-D-2 burn 2 | ||
| 1818? | Blok D-2 MECO-2 | 170? x 130000? x 50.8? | |
| 1820? | Blok-D-2 sep | ||
| 1820? | ADU burn, solar orbit insertion | ||
| 1988 Jul 21 | TCM 1 9.3m/s | ||
| 1988 Nov 1 | one transmitter out of order | ||
| 1989 Jan 23 | TCM 2 (Earth range 177Mkm) 20.8m/s | ||
| 1989 Jan 24 | 2030? | Enter Mars sphere | |
| 1989 Jan 29 | 1255 | Mars orbit insertion 815.1m/s | 79h 37m 867 x 81357 x 0.9 |
| 1989 Feb 12 | 1300 | OTM 114.6m/s | 86.5h 6408 x 81346 x 0.9 |
| 1989 Feb 18 | 1406 | ADU burn 722m/s | 8h 6145 x 6409 x 1.26 |
| 1989 Feb 18 | ADU sep | ||
| 1989 Feb 21 | First Phobos imaging, 860 km | ||
| 1989 Feb 28 | Pass 320 km from Phobos | ||
| 1989 Mar 7 | 1226 | TCM 37.6m/s with OA's DU | |
| 1989 Mar 15 | 1420 | TCM 1.0m/s | |
| 1989 Mar 21 | 1446 | TCM 39.7m/s | 200 km from Phobos, sync |
| 1989 Mar 25 | 191 km from Phobos | ||
| 1989 Mar 26? | TCM? | ||
| 1989 Mar 27 | 1159 | Final Phobos imaging | |
| 1989 Mar 27 | 1650 | Faint signal received, s/c tumbling | |
| 1989 Mar 27 | end of ops | ||
Payload:
- ADU = Avtonomnaya Dvigatel'naya Ustanovka
- OPB (Orbiter/Lander Unit)
- APEX gamma ray bursts
- LET 0.9-75 MeV cosmic rays
- SLED 20-140 keV e, 20 -3400 keV p, 0.1-3.4 MeV alpha
- Fregat TV system
- Radiometer
- Photometer
- IR spectrometer
- FGMM-1 magnetometer
- Lima-D laser
- Mass spectrometer
- Dion Kr ion gun, Fobos 2 only
- DPS Lander probe (LAS)
- Radio beacon
- Seismometer
- XR flourescence spectrometer
- Razrez penetrometer
- Panoramic TV system
- Hopper probe (PPS)
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