Friday, January 4, 1991
Tuesday, January 1, 1991
Phobos 1
1988-058A
The Fobos missions were the first of the fourth generation planetary probes, using a bus derived from both the 4V planetary probe and the E-8 lunar probe. Work began on the project in 1976. The first Fobos spacecraft, 1F No. 101, was launched on 1988 Jul 7 aboard a Proton-K. The three-stage Proton placed Fobos and the specially modified 11S824F (Blok-D-1) fourth stage on a suborbital trajectory. The Blok-D-1 ignited to enter parking orbit, and then coasted until a second burn. The second burn left Fobos-1 in a highly eccentric orbit, and solar orbit insertion was completed using the Fobos spacecraft's own ADU propulsion unit.
On 28 Aug 1988 an error was made in a command to switch on the gamma ray spectrometer; the command actually sent instructed Fobos 1 to turn off its orientation and stabilization system. With the solar panels away from the Sun, the batteries ran down. On the next comms pass on Sep 2, nothing was heard from the probe, although loss of contact was not officially admitted until 1988 Nov 3.
| Fobos-1 | |||
| Date | Time | Event | Orbit |
|---|---|---|---|
| 1988 Jul 7 | 1738:04 | Launch by Proton-K | KB |
| 1747 | Stage 3 MECO | ||
| 1747 | Stage 3 sep | ||
| 1988 Jul 7 | 1753:50 | Blok-D-2 burn (T+15:46) 95s | |
| 1755:25 | Blok-D-2 cutoff (T+17:21) | 88.13 169 x 197 x 51.5 | |
| 1810 | Equator crossing southbound | ||
| 1841 | Perigee of post-sep D-2 orbit | ||
| 1847? | SOZ units sep | ||
| 1847? | Blok-D-2 burn 530s? | ||
| 1854 | SOZ eq crossing north | ||
| 1856? | MECO-2 | ||
| 1900? | Blok-D-2 sep | ||
| Blok D-2 venting | 2628 x 130504 x 50.8 | ||
| 1905? | ADU burn, solar orbit insertion | ||
| Control to OKIK-16/Yevpatoria | |||
| 1988 Jul 16 | TCM-1 8.9m/s | ||
| 1988 Aug 18 | Control to TsNIIMash/Kaliningrad | ||
| 1988 Aug 28 | Command error | ||
| 1988 Sep 1 | failed to respond to commands | ||
| 1989 Jan 23 | Mars flyby | ||
Payload:
- Terek Solar X-ray spectrometer
- SUFR Solar UV
- IPNM Neutron radiation study
- GRUNT Penetrating radar
- ADU Propulsion unit
- DPS Lander
Phobos 2
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)
May 13,2026
https://planet4589.org/space/jsr/back/news.855.txt
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