Tuesday, January 1, 1991

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)


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