Saturday, January 15, 1994

OGO 2

  1965-081A


 The first POGO (Polar Orbiting Geophysical Observatory) was launched by Thrust Augmented Thor Agena D from Vandenberg on 1965 Oct 14. The orbit was 104.4 min, 415 x 1517 km x 87.4 deg. This orbit was significantly higher than the planned 97.33 min, 333 x 932 km x 86.0 deg one beacuse of a radio guidance failure. Attitude control was again lost early in the mission, on Oct 23, and the satellite was declared a failure. Nevertheless it sent back data until 1967 Nov 1 when it was shut down. It was reactivated for two weeks in 1968 Feb, then put on standby until 1971 Nov 1. The satellite reentered on 1981 Sep 17.


OGO 2 
 

DateTimeEventOrbit  

1965 Oct 14  1311:55  Launch by TAT Agena D  V 75-1 Pad 1 
 1313:00  Castor sep (T+1:05) 
 1314:25  Thor MECO, LOX depletion (T+2:30) 
 1314:34  Thor VECO (T+2:39) 
 1314:42  Thor sep (T+2:47) 
 1316:04  Agena 6801 burn (T+4:09) 
 1320:05 Agena MECO (T+8:10) 
 1320:17  Pitch sensor operation 
  Agena sep 
   104.00 411 x 1454 x 87.35 (VCR) 
 1700   104.41 415 x 1517 x 87.43 (RAE) 
1965 Oct 23   Attitude control lost 
1967 Nov 1   Deactivated 
1968 Feb   Reactivated 
1968 Jun Standby mode
1970 Sep 1  0000   102.36 409 x 1333 x 87.3 (RAE) 
1971 Nov 1   Deactivated 
1981 Sep 17   Reentered 

The 1992 CIA World Factbook

 https://www.gutenberg.org/files/48/48.txt

Friday, January 14, 1994

Kosmos 2108

 1990-109A



Kosmos-2108 
 

DateTimeEventOrbit  

1990 Dec 4  1830:00 Launch by Soyuz  PL 
 1838  Blok-I sep 
1990 Dec 4.8   89.57 189x317x62.8 
1990 Dec 5.8   89.52 188x312x62.8 
1990 Dec 7.2   89.73 186x336x62.8 from 89.52 188x312 
1990 Dec 17.1   89.26 173x302x62.8 from 88.82 171x261 
1990 Dec 20   SpK-1 fiducial 
1990 Dec 21.9   89.89 165x373x62.8 from 88.83 165x268 
1990 Dec 25.92   90.04 174x378x62.8 from 89.56 160x345 
1991 Jan 1   89.21 168x302x62.8 from 89.66 169x346 
1991 Jan 6.2   89.11 165x294x62.8 from 88.78 161x267 
1991 Jan 9.3   89.78 184x342x62.8 from 88.78 159x268 
1991 Jan 10   SpK-2 fiducial 
1991 Jan 16.9   89.58 196x311x62.8 from 89.31 181x299 
1991 Jan 19.6   89.96 178x366x62.8 from 89.50 194x304 
1991 Jan 20.9   89.11 175x285x62.8 from 89.90 177x361 
1991 Jan 26.0    88.96 174x271x62.8 from 88.50 162x237 
1991 Jan 28.6    88.58 166x242x62.77 
1991 Jan 29 
 1858? Deorbit 
 1914? Entry 
 1926? Landing 

Wednesday, January 12, 1994

Kosmos 1923

 1988-015A


Two-tone telemetry; Hi res satellite


Kosmos-1923
 

DateTimeEventOrbit  

1988 Mar 10  1030  Launch by Soyuz  PL 
 1034  Blok-I burn 
 1038  Blok-I sep 
1988 Mar 10   89.48 194x305x72.8 
1988 Mar 11    89.65 227x288x72.8 
1988 Mar 14  90.28 227x349x72.9 
1988 Mar 17    90.26 226 x 347 x 72.9 
1988 Mar 20   
89.35 221 x 263 x 72.9 
1988 Mar 22   
 0532?  Deorbit 
 0542?  PO sep 
 0550?  Entry 
 0607?  Landed 

Monday, January 10, 1994

Venera 2A

  1962-040A


2MV-1 No. 1 was the first of a new generation of planetary probes developed by OKB-1. The 8K78 rocket was modified with an improved 8D727K engine in the Blok A stage and a longer fairing. The Blok-L stage failed to work correctly, stranding the satellite in orbit. One of the four BOZ ullage motors failed to ignite, causing the vehicle to tumble. The Blok-L S1.5400A1 engine shut down after 45s of a planned 240s burn. The spacecraft would have carried out a Venus landing if successful.


2MV-1 No. 1 
 

DateTimeEventOrbit  

1962 Aug 25  0218:45 Launch by 8K78  KB 
 0223  Blok-A sep 
 0227  Blok-I sep  173 x 252 x 64.88 
 0319:35  BOZ burn 
 0319  BOZ motors failed 
 0319  Blok-L burn 
 0319  Tumbling 
 0319  Blok-L cutoff at 45s 
1962 Aug 28   Reentered 

Payload:

  • 2MV-1 Venus landing capsule

Space Year 1991: The Complete Record of the Year's Space Events

 https://welib.org/md5/af231b19c1536d28a281c3a47a18412d

Kosmos 1833

 1987-027A


Kosmos-1833 was EPN No. 03.694, a Tselina-2 test launch.


Kosmos-1833 
 

DateTimeEventOrbit  

1987 Mar 18  0830:00 Launch by Zenit-2  KB 
 0832:23  T+2:23 St 1 MECO 
 0832:25  T+2:25 Stage 1 sep 
 0832:25  T+2:25 Stage 2 burn 
 0832:40  T+2:40 GO sep 
 0836:42 T+6:42 Stage 2 MECO 150? x 850? x 71.0 
 0845? T+15m? Stage 2 VECO 
 0845?  Stage 2 sep motor covers 
 0845?  T+15m? Stage 2 sep 
1987 Mar 18  (27B) 101.78 839x847x71.0 
1987 Mar 18  101.92 848x851x71.0 
1987 Mar 23  849x853x71.01 
1987 Mar 29 end of ops

Monday, January 3, 1994

Arabsat 1B

 1985-048C


The second Arabsat was launched on mission 51-G. The satellite was leased to ISRO in 1989.


Arabsat 1B 
 

DateTimeEventOrbit  

1985 Jun 18  1356:56  Arabsat deploy from OV-103 
 1442  PAM-D burn 
 1443  PAM-D burnout 
 1445  PAM-D sep 
1985 Jun 18    628.69 382 x 35481 x 26.7  
1985 Jun 19    628.85 383 x 35488 x 26.7  
1985 Jun 19   LAM-1? 
1985 Jun 21  1100? LAM-2  
1985 Jun 22    1424.20 35268 x 35838 x 0.1 GEO 16.2E+3.0E 
1985 Jun 25   mv in  
1985 Jun 26    1436.25 35779 x 35800 x 0.1 GEO 26.0E+0.05W 
1985 Jul 9    1436.04 35720 x 35850 x 0.1 GEO 26.1E 
1986 Dec 1    1436.04 35549 x 36021 x 0.1 GEO 26.1E 
1989 Jan 25    1436.07 35768 x 35804 x 0.1 GEO 26.1E 
1989 Aug 29    1436.02 35675 x 35894 x 0.1 GEO 26.2E 
1989 Oct 1   ISRO lease 
1990 Apr 23    1436.07 35736 x 35835 x 0.1 GEO 25.8E 
1990 Aug 25    1436.03 35734 x 35835 x 0.1 GEO 26.1E 
1991 May 31    1436.02 35748 x 35821 x 0.1 GEO 26.1E 

Kosmos 422

  1971-046A


Kosmos-422 was launched in May 1971 to join the Tsiklon navsat constellation.


Kosmos-422 
 

DateTimeEventOrbit  

1971 May 22  0051:31?  Launch by 11K65M  PL  
 0055?Stage 2 burn  
 0059?  Stage 2 cutoff 
 0153?  Stage 2 burn 2 
 0154? Stage 2 sep  
1971 May 23  1430   105.10 988 x 1014 x 74.03

Saturday, January 1, 1994

Raduga 15

 1984-063A


Raduga (Gran') No. 27 was launched to the 128E position in Jun 1984.


Raduga No. 27L
 

DateTimeEventOrbit  

1984 Jun 22  0020 Launch by Proton-K  KB 
 0029 Stage 3 sep 
 0137? DM burn 1 
 0653? DM burn 2 
 0657? DM sep 
1984 Jun 22    1397.73 35016 x 35047 x 1.3 GEO 97.1E+9.9E 
1984 Jun 25    1425.07 35520 x 35620 x 1.3 GEO 122.6E+2.8E 
1984 Jun 30    1435.74 35752 x 35807 x 1.3 GEO 127.0E 
1984 Aug 5    1436.07 35763 x 35808 x 1.2 GEO 128.5E 
1985 Jul 2    1436.34 35781 x 35801 x 0.3 GEO 128.1E 
1986 Dec 10    1436.17 35786 x 35789 x 1.0 GEO 128.5E 
1988 Apr 7   last mv  1436.36 35778 x 35804 x 2.3 GEO 127.0E+0.05E 
1988 Aug 7    1436.21 35782 x 35795 x 2.6 GEO 128.7E+0.03W 
1988 Sep?   retired 
1988 Oct 8    1436.67 35782 x 35813 x 2.7 GEO 123.4E+0.15W 
1991 Apr 14    1435.84 35758 x 35805 x 5.1 GEO 127.9E+0.06E 
1992 Aug 25    1436.43 35703 x 35882 x 6.2 GEO 18.7E+0.09W 

Giotto

 1985-056A


Giotto was based on the Geos bus and built by the same BAe/STAR consortium. The probe was built from the Geos engineering model. ESA controlled Giotto from ESOC. Flyby velocity was 68.4 km/s with 596 km closest approach.


Giotto 
 

DateTimeEventOrbit  

1985 Jul 2  1123:13  Launch by Ariane I  CSG 
  T+2:25 St 1 MECO 
  T+2:30 Stage 2 burn 
  T+4:14 Fairing 
  T+4:51? St 2 sep 
  T+4:55? Stage 3 burn 9:21?  
 1137 T+14:16? Stage 3 MECO 
 1138?  Stage 3 sep 203 x 35421 x 7.0 
 1139  Perigee 
 1145  AOS by Malindi 
 1650  Spin axis slew 
1985 Jul 2  1700?  Apogee 1  
1985 Jul 2  2110  Perigee 1, 202 km  
 2210  Perigee 1 from TLE 
1985 Jul 3  0230?  Apogee 2 
 0844  Perigee 2 from TLE 
 1400?  Apogee 2 
  Spinup 
 1914  Perigee 3 from TLE 2 
 1918  Perigee 3 from TLE 1 
 1923:47  Mage 1S perigee burn 1.40km/s Solar orbit 

 

1924:42  Burnout (55s) 
1985 Jul 4  0333? Pass EL1:4 
1985 Jul 4  0730  Nozzle cover closed 
1985 Jul 6  0947  HGA release 
  Begin cruise, mass 578.5 kg 
1985 Jul 8  0230?  Pass L1 
1985 Jul 15   3.43Mkm range 
1985 Aug 26   TCM-1, 7.27m/s, 92 min 
1985 Oct 2   Range 20.235Mkm to Earth 
1986 Jan 24   Antenna lock loss, recovered by DSN 
1986 Mar 12  0053  TCM 2.5m/s 
 0125  TCM complete 
1986 Mar 13  1816  (ERT) PKS gets signal 
1986 Mar 13   Encounter P/Halley at 0.90AU, vrel 68.4 km/s 
  Mass 573.9 kg 
 2356:58  First bumper shield penetration 
1986 Mar 14  0002:52  Last image 
 0002:52  Hit by 1g of particles 
 0002:55  Loss of signal 
1986 Mar 14  0003:02  Passed 596 km from nucleus 
 0003:19  Signal recovered 
 0004:34  Spacecraft nutating 
 0034:58  Spacecraft recovered 
1986 Mar 19   TCM 4h30m, 63 m/s, 19 kg 
1986 Mar 20   TCM 4:10min, 46m/s, 14 kg 
1986 Mar 21   TCM 16min, 2.6m/s, 1 kg  0.833 yr 0.733 x 1.04 AU 
1986 Apr 1   TCM 1.5m/s  
1986 Apr 2   TCM 1.3m/s? 
1986 Apr 2  0225  Deactivated 
1990 Feb 20   Reactivated by DSN/Madrid, R=102.9 Mkm Rdot=14.54km/s Vsun=37.36km/s 
1990 Feb 21   HGA despin attempts 
1990 Feb 25  1745 ESOC resumes control 
  HMC and NMS deactivates 
1990 Mar 3   Perihelion 
1990 Mar 13   TCM to retarget for Grigg-Skjellerup 
1990 Jul 2  1001:18  Flyby Earth, 22730 km over Australia  390d? 
  Inc = 45 deg 
1990 Jul 16   TCM 0.5m/s 
1990 Jul 22   Hibernation mode 
1992 Apr   Reactivated 
1992 May 22   TCM, 3.5m/s targeting to 800 km 
1992 Jul 1   Science instruments on 
1992 Jul 8   TCM, 2m/s targeting to 200 km 
1992 Jul 10  1519  Encounter P/Grigg-Skjellerup 200 km, at 1.01 AU from Sun LT=24min 
  Rel 13.99 km/s 
1992 Jul 11   Experiments off 
1992 Jul 21   TCM, target to Earth swingby, 4h burn 33m/s 
1992 Jul 23   TCM correction 3m/s 
1992 Jul 23   In hibernation mode 

Phases of Gravity

 https://welib.org/md5/3deda758a4b4bdd0d1210c4c2a0d9854

Seventeen: July 1993

 https://welib.org/md5/2e03e7b49585a08e52865bdb57b952c7

Friday, December 31, 1993

Kosmos 1732

 1986-015A



Kosmos-1732 
 

DateTimeEventOrbit  

1986 Feb 11  0656 Launch by 11K68  PL 
  T+2:00 St 1 sep 
  T+3:33 GO sep 
  T+4:38 St 2 sep 
  T+5:19 S5M burn 1, 
 0702  T+6:48 S5M MECO-1  90? x 1502 x 73.6 
  T+49:37 BOZ burn 
  T+51:15 S5M MES2  
  T+51:33 S5M MECO2 
 0748  T+52:03 S5M sep 
1986 Feb 11   1480x1525x73.6 
1988 Jul  end of ops 

Monday, December 27, 1993

Crystal 8

 1987-090A


The next KH-11 went up in Oct 1987 and was given the official designation USA 27. It flew in the 1300 LTDN east plane orbit. 


CRYSTAL 8 
 

DateTimeEventOrbit  

1987 Oct 26  2132  Launch by Titan 34D  V SLC4E 
 2133  Core engines on (T+1:47) 
 2133  SRM jettison (T+1:56) at 39 km  
 2136?  T+4:34? Stage 1 sep  
 2136?  Stage 2 ignition (T+4:34?) 
 2136?  Fairing sep (T+4:46?) 
 2139?  Stage 2 cutoff (T+8:09?) 
 2140?  Stage 2 sep (T+8:21?)   
   153 x 1029 x 97.8 (UN) 
   143 x 1018 x 97.8 (UN, 90B) 
1990 May 28   97.54 307x973x97.96 
1991 May 25   97.43 339x932x97.75 
1991 Jul 9    97.26 322x932x97.70 

Saturday, December 25, 1993

Progress 42

 1990-041A


The final 7K-TG spacecraft was 11F615A15 No. 150, named Progress-42 after launch. It carried 2409 kg of cargo to Mir in May 1990.


Progress-42 
 

DateTimeEventOrbit  

1990 May 5  2044:01  Launch by Soyuz-U  KB 
 2053  Blok I sep 
 2130   88.81 188 x 243 x 51.63 
1990 May 6  0500 89.97 220 x 324 x 51.62 
1990 May 7  0230   91.76 323 x 398 x 51.62 
 2245Docked with Mir, Kvant DP2 
1990 May 8  0230   92.38 383 x 398 x 51.61 
1990 May 26  2130   92.29 379 x 393 x 51.61 
1990 May 27  0708Undocked from Mir 
   92.28 378 x 393 x 51.62 
 1145Deorbited 
 1227 Reentered 

Kosmos 1824

 1987-021A


Kosmos-1824 continued the Kobal’t legacy into the spring of 1987.


Kosmos-1824 
 

DateTimeEventOrbit  

1987 Feb 26  1530 Launch by Soyuz  PL 
 1538  Blok-I sep 
1987 Feb 26    (21B) 166x334x67.1 d Mar 4 
1987 Feb 26    165x335x67.1 
1987 Mar 1    89.47 164 x 331 x 67.1 
1987 Mar 6    89.18 160 x 307 x 67.1 
1987 Mar 8   Orbit raise 89.51 168 x 332 x 67.1 
1987 Mar 12    89.28 164 x 313 x 67.1 
1987 Mar 16   Orbit raise  89.76 179 x 345 x 67.1 
1987 Mar 18   SpK-1 fiducial 
 0427?  Deorbit 
 0435?  Entry 
 0449?  Landed
1987 Mar 19    89.63 177 x334 x 67.1 
1987 Mar 20   
89.18 168 x 299 x 67.1 
1987 Mar 21   
89.25 169 x 305 x 67.1 
1987 Mar 27    88.65 160 x 255 x 67.1 
1987 Mar 28   
89.48 175 x 321 x 67.1 
1987 Mar 30    89.33 174 x 308 x 67.1 
1987 Mar 31   
89.11 173 x 287 x 67.1 
1987 Apr 5    88.73 168 x 255 x 67.1 
1987 Apr 6 
89.77 173 x 352 x 67.1 
1987 Apr 7 SpK-2 fiducial 
 2229?  Deorbit 
 2238?  Entry 
 2253?  Landed
1987 Apr 10    89.44 173 x 319 x 67.1 
1987 Apr 12 
89.21 153 x 317 x 67.1 
1987 Apr 14    88.74 149 x 275 x 67.1 
1987 Apr 15   
89.17 175 x 290 x 67.1 
1987 Apr 15    89.11 174 x 286 x 67.1 
1987 Apr 16   
89.40 179 x 309 x 67.1 
1987 Apr 22    89.06 175 x 281 x 67.1 
1987 Apr 23  
 1802?  Deorbit 
 1816? Entry 
 1831? Landed

Soyuz T-11 (Jupiter)

 1984-032A


11F732 No. 17L was launched in Apr 1984 with the Soviet-Indian crew and named Soyuz T-11.


    Crew

  • Komandir Pol. Yuriy Malyshev, VVS

  • Bortinzhener Gennadiy Strekalov, NPO Energiya

  • Kosmonavt-issledovatel' Sqn. Ldr. Rakesh Sharma, Indian Air Force.


Soyuz T-11, Flight 1 
 

DateTimeEventOrbit  

1984 Apr 3  1309  Launch by Soyuz-U  KB 
 1311 Blok-BVGD sep 
 1313  Blok-A sep  
 1317  Blok-I cutoff 
 1317  Blok I sep 
 1400   88.62 195 x 223 x 51.6 
   227 x 270 x 51.6 
1984 Apr 4    222 x 274 x 51.6 
 1431  Docked with Salyut-7 +X 


    Crew

  • Komandir Pol. Leonid Kizim, VVS

  • Bortinzhener Vladimir Solov'yov, NPO Energiya

  • Kosmonavt-issledovatel' Oleg Atkov, IMBP


Soyuz T-11, Flight 2 
 

DateTimeEventOrbit  

1984 Apr 13    283 x 293 x 51.6 
  Hatch closed 
 1027  Undocked Salyut-7 +X 
 1102  Redocked Salyut-7 -X 


    Crew

  • Komandir


Soyuz T-11, Flight 3 
 

DateTimeEventOrbit  

1984 Oct 2  0740?  Undocked Salyut-7 -X 
 0842?  BO sep 
 1001? Deorbit 
 1005?  DO CO  
 1028?  PAO sep 
 1034?  Entry 
 1057  Landed 

November 20,2006

  https://en.wikipedia.org/wiki/Association_football