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 
 

DateTimeEventOrbit  

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 
 

DateTimeEventOrbit  

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