Tuesday, December 26, 1995

STS-52 (Columbia)

 1992-070A


STS-52 was launched on 1992 Oct 22 with the Italian LAGEOS-2 geodetic satellite and the USMP-1 cargo bay microgravity payload.

The IRIS sunshade was opened at 1334 on Oct 23 and spinup began at 1338. The IRIS/Lageos/LAS spacecraft was deployed at 1357:20.

On Oct 24 the Canadian Target Assembly was unberthed for a simulation of Space Station PIT (Pre Integrated Truss) assembly and the Space Vision System. On Oct 29 the CTA was again unberthed by the RMS. At about 1250 the astronauts hit a problem when the RMS refused to reberth the CTA while running in single joint mode. It was finally reberthed at 1325. The next day it was taken out again for the SVS-9, 5, 6 tests.

On Oct 30, the orbit was lowered again. In the OMS-6 burn, the left engine was used using fuel from the right pod, the first time such a crossfeed had been used since it was tested on STS-2 in 1981.


    STS-52 Crew

  • Commander James D. Wetherbee, Cdr. USN

  • Pilot Michael A. Baker, Capt USN

  • Mission Specialist 1 C. Lacy Veach, NASA

  • Mission Specialist 2 William M. Shepherd, Capt. USN

  • Mission Specialist 3 Tamara E. Jernigan, PhD., NASA

  • Payload Specialist 1 Steven Glenwood MacLean, PhD., CSA


STS-52 
 

DateTimeEventOrbit  

1992 Sep 21    VAB/1 
1992 Sep 26   Rollout  LC39B 
1992 Oct 22  1709:32  main engine ignition
 1709:39  Launch  LC39B 
 1711:42  SRB sep 
 1718:11  MECO  88.22 69 x 303 x 28.5 (OMS dV) 
 1718:29  ET Sep 
 1719:30? RCS burn for ET photo DTO 312 
 1749:34  OMS 2 2:17 68m/s 90.58 301 x 303 x 28.46 
 1751:52  OMS 2 CO 
 1838  PLBD open 
1992 Oct 23   RMS uncradle 
 1357:24  Lageos deploy  
 1412:07  OMS-3R (16s) sep 4m/s 
 1610  RMS cradle 
 1628:03  OMS-4R lower orbit 13s 3m/s 
 1714:38  OMS-5L lower orbit 31s 8m/s  90.30 285 x 293 x 28.5  
 1715:10  OMS-5 CO 
1992 Oct 24  2015?  RMS grapple CTA  
 2039  RMS unberth CTA  
 2047  RMS reberth CTA  
 2048.15  RMS unberth CTA  
 2210:25  RMS reberth CTA  
 2212:20  RMS unberth CTA  
 2217?  RMS reberth CTA  
 2220?  RMS ungrapple CTA  
 2229  RMS berthed 
1992 Oct 25  2330   90.31 285 x 293 x 28.46 
1992 Oct 29  1021  RMS grapple CTA  90.32 285 x 294 x 28.5 
 1021  RMS unberth CTA  
 1211  Berthing in progress? 
 1250?  CTA reberth problem 
 1325  RMS reberth CTA; relatch 1338 
 1357  RMS ungrapple CTA 
 1409  RMS recradle 
 2100   90.31 285 x 294 x 28.46 
1992 Oct 30   RMS uncradle 
  RMS grapple CTA  
  RMS unberth CTA 
 1230?  RMS reberth CTA 
  RMS ungrapple CTA 
 1308:55 OMS 6L (1:30) 22m/s lower orbit  211 x 283 x 28.5 
 1310:25 OMS 6 CO 
 1355:39  OMS 7L 1:23 22m/s 
 1357:02  OMS 7 CO 
 1411   88.76 210 x 216 x 28.5 
 1605  RMS uncradle 
 1626  RMS grapple CTA 
 1629  RMS unberth CTA (OGLOW) 
 1834  RMS reberth CTA 
  RMS ungrapple CTA 
  RMS cradle 
1992 Oct 31   RMS uncradle 
 0854  RMS grapple CTA  88.73 208 x 215 x 28.5 
 0857  RMS unberth CTA 
 1006 RMS deploy CTA 
  RCS sep burn 
  RCS sep 2 
 1048  RCS sep 3 
 1245  RMS recradle  88.73 207 x 215 x 28.5  
 2100   88.71 206 x 214 x 28.46 
1992 Nov 1  0830  USMP-1 deactivate 
 1032  PLBD close 
 1311:59  OMS DO (2:07) 68m/s   
 1314:06  OMS DO CO 
 1333:52  Entry interface 
 1405:38  Gear down 
 1405:52  Landing  RW33 KSC  
 1406:07  Drag chute deploy 
 1406:11  NGTD 
 1406:42  Drag chute jettison 
 1406:53  Wheels stop 
 1730OPF 

Town and Country: May 1995

 https://welib.org/md5/f2b376ced27ffd1509fcc07e10c90dbf

Excalibur

 https://welib.org/md5/6218474fde445792fe07851e808d0f2a

Progress M-22

 1994-019A


Progress M No. 222 was launched in Mar 1994 as Progress M-22. Mass after orbit insertion was 7103 kg.


Progress M-22 
 

DateTimeEventOrbit  

1994 Mar 22  0454:12  Launch by Soyuz-U 
 0503:00  Blok-I sep  88.50 192 x 237 x 51.6 (AVM) 
   186 x 220 x 51.6 
 0833s  TCM1 
 0933s  TCM2 
1994 Mar 24  0430s  TCM3 
 0515s  TCM4 
 0639:37 Docked with Mir Kvant DP2 
1994 May 23  0058:38  Undocked from Mir 
 0352  TDU burn, deorbit 
 0440  Reentered over 51 01 S 114 59 W

Monday, December 25, 1995

Kosmos 2077

 1990-042A



Kosmos-2077 
 

DateTimeEventOrbit  

1990 May 7  1839:59 Launch by Soyuz  PL 
 1848  Blok-I sep 
1990 May 7  89.64 183x329x62.85 
1990 May 8  89.63 187x325x62.84 
1990 May 9  90.62 222x387x62.84 
1990 May 14  90.00 174x374x62.8 from 90.62 223x386 
1990 May 18  89.00 160x289x62.8 from 89.43 164x327 
1990 May 20  88.94 168x276x62.8 from 88.68 154x263 
1990 May 22  89.76 183x342x62.8 from 88.73 164x259 
1990 May 27   SpK-1 fiducial 
1990 May 28  89.61 196x314x62.8 from 89.20 173x296 
1990 Jun 5.1   89.67 221x294x62.8 from 89.27 189x287 
1990 Jun 5  89.08 189x268x62.9 from 89.67 221x294 
1990 Jun 10  89.67 186x392x62.9 from 89.03 171x281 
1990 Jun 16   SpK-2 fiducial 
1990 Jun 19  89.17 177x290x62.8 
1990 Jun 21  89.63 186x325x62.8 from 89.03 174x279 
1990 Jul 2  88.92 161x280x62.8 from 88.72 164x257 
1990 Jul 3  88.77 158x268x62.8 
1990 Jul 4  88.55 155x250x62.8 
1990 Jul 6 
 1755?  Deorbit 
 1810?  Entry 
 1824?  Landed

Kosmos 952

 1977-088A


Kosmos-952 may have been one of the first US-A satellites built at KB Arsenal to fly, replacing OKB-52 as contractor.


Kosmos-952 
 

DateTimeEventOrbit  

1977 Sep 16  1425  Launch by Tsiklon-2 Baikonur
 1427  Stage 1 sep 
 1429  Stage 2 sep  -800? x 265 x 65 
 1439? DU burn  
 1449? Stage 2 reentry 
1977 Oct 8  1541   104.13 905 x 1000 x 64.9 
1977 Sep 16   89.7 251x265x65.0 
1977 Oct 7  1517   89.64 249 x 263 x 65.0 
1977 Oct 8 1150? reactor sep  218? x 996? 
 1231?  Burn 2 
1977 Oct 8  1541   104.13 905 x 1000 x 64.9 
1977 Oct 9   104.1 910x998x64.9 

Sunset Dreams

https://welib.org/md5/4492b42c4cee7514cb64ab6117e6d411

Sunday, December 24, 1995

Himawari 3

 1984-080A


The NEC/Hughes GMS-3A satellite was launched in Aug 1984 and became Himawari 3. The 281 kg satellite was 3.45 m long, 2.16m diameter and had 41 kg of prop. It included a jettisonable radiometer cover.


Himawari 3 
 

DateTimeEventOrbit  

1984 Aug 2  2030 Launch by N-2  TNSC 
  T+0:38 SRM 7-9 on 
  T+1:15 SRM 1-9 sep 
  T+4:32 MECO  
  T+4:40 St 1 sep 
 2034  T+4:46 Stage 2 burn 
  T+5:00 Fairing sep
 2041  T+11:07 SECO 
 2053 T+23:07 SES-2 7s 
 2053 T+23:14 SECO-2 
 2054  T+24:14 Spinup 
 2054 T+24:22 Stage 2 sep 
 2054  T+24:54 Stage 3 burn 37s? 
 2055 T+25:38 Stage 3 burnout after 44s 
 2056  T+26:54 Stage 3 sep 
1984 Aug 3  0300? Apo 1 
 0800? Peri 1 
 1300? Apo 2 
 1830? Peri 2 
1984 Aug 4  0000? Apo 3  
 0530? Peri 3 
 1100? Apo 4 at 178E 
1984 Aug 4  1100? Star 27 AKM at 4th apo 
1984 Aug 4  1105? Star 27 ejected 
1984 Aug 4    1451.05 35730 x 36427 x 1.9 GEO 178.9W+3.7W 
1984 Aug 13    1450.24 35784 x 36341 x 1.9 GEO 147.0E+3.5W 
1984 Aug 15?  Radiometer cover jettison 
1984 Aug 15?  mv in 
1984 Sep 7    1436.17 35782 x 35793 x 1.8 GEO 140.3E 
1984 Sep 27   Begin operational data 
1985 Jan 26    1436.12 35784 x 35789 x 1.4 GEO 140.3E 
1986 Jan 25    1436.20 35785 x 35792 x 0.5 GEO 139.8E 
1987 Jan 5    1436.02 35784 x 35786 x 0.4 GEO 140.0E 
1988 Feb 11    1436.04 35782 x 35788 x 0.7 GEO 140.1E 
1989 Feb 11    1436.26 35786 x 37593 x 0.8 GEO 139.7E 
1989 Dec 8    1436.34 35787 x 35795 x 1.4 GEO 139.0E+0.07W 
1989 Dec?   Move to 120E 
1990 Feb 14    1436.15 35786 x 35789 x 1.6 GEO 120.0E 
1991 Jan 1    1436.09 35784 x 35788 x 2.4 GEO 120.2E 
1993 Feb 22    1436.15 35782 x 35792 x 4.2 GEO 120.1E 

Journal of the British Interplanetary Society: May 1995

 https://welib.org/md5/c635a9306612ff2de9d73f90e7ca2063

HEOS 1

  1968-109A


The Highly Eccentric Orbit Satellite was built for ESRO by Junkers Flugzeug und Motorenwerke AG.

HEOS-1 was launched in Dec 1968 by a Delta E1 from Cape Kennedy. On 1969 Mar 18 the 8 kg S-16 barium capsule was ejected and ignited as the first high altitude chemical release.


HEOS 1 
 

DateTimeEventOrbit  

1968 Dec 5  1855:00  Launch by Delta DSV3E-1 CK LC17B 
  T+0:38 SRM burnout  
  T+1:00 SRM sep 
 1857:29 T+2:29 MECO 
  T+2:34 St 1 sep 
 1857:34 T+2:34 SES-1 6:28 
  T+2:46 Fairing sep 
 1904:02 T+9:02 SECO-1 387 km  
  T+48:20 Spinup 
 1943:35 T+48:35 St 2 sep  176 x 792 x 28.3 
 1943:35  T+48:35 FW4D ignition 32s, 446 km 
 1944:07  T+49:06 FW4D burnout, 457 km 
 1944:36  T+49:36 Despin weights sep
 1945:06  T+50:06 FW4D sep 
   6750.0 418 x 223440 x 28.3 
1968 Dec 6  1320?  Pass EL1:4 
1968 Dec 10    6699.72 421 x 222269 x 28.3 
1969 Mar 18    2302 x 220406 x 31.7 
1969 Mar 18  0439:51  S-16 capsule ejected 
  HEOS orbit  2298 x 220341? x 31.7 
  S-16 orbit  2358? x 221251? x 31.7 
 0720:52  Barium cloud ignited, alt 75000 km 
1970 Mar 19    6704.14 12444 x 210549 x 52.6 
1970 Nov 7    6704.20 20020 x 202775 x 60.5 
1970 Dec 5    6704.61 21119 x 201686 x 61.8 
1975 Oct 28   End of transmissions 

Progress M-11

 1992-004A


Progress M (7K-TGM) No. 212 carried an experiment from Payload Systems and a CNES microaccelerometer.


Progress M-11 
 

DateTimeEventOrbit  

1992 Jan 25  0750:17  Launch by Soyuz-U  KB 
 0759  Blok-I sep 
   190 x 245 x 51.6 
1992 Jan 27  0930:43  Docked with Mir 
1992 Mar 12  0843:40  Undocked 
 1511:25Deorbited over Pacific 
 1547:32Reentered 

Familiar Studies of Men and Books

 https://www.gutenberg.org/files/425/425-0.txt

Peterson's Greetings from High School 1991

 https://welib.org/md5/ab0393891411eac08865013ac2cc71cb

Soyuz T-3

 1980-094A


Soyuz 7K-ST No. 8L was the first operational use of the Soyuz T spaceship, with its full complement of three crew members. Leonid Kizim, Oleg Makarov and Gennadiy Strekalov were launched to Salyut-6 to carry out a series of repairs and technology experiments on a short two week mission.


Soyuz T-3, Flight 1 
 

DateTimeEventOrbit  

1980 Nov 27  1418:28  Launch by Soyuz-U  KB 
 1420  Blok BVGD sep 
 1422  Blok A sep 
 1426  Blok I MECO 
 1427Blok I sep 
 1500
88.76 196 x 236 x 51.62 
   88.60 188 x 266 x 51.6 
   89.61 255 x 260 x 51.6 
1980 Nov 28  1554  Docked with Salyut-6 


Soyuz T-3, Flight 2 
 

DateTimeEventOrbit  

1980 Dec 8  1045Test burn 
1980 Dec 10  0439Crew to Soyuz, hatch closed 
 0610  Undocked  284 x 353 x 51.6 
 0710? BO sep 
 0840? Deorbit 
 0844?  DO CO 
 0854? PAO sep  -90? x 344 x 51.6 
 0903?  Entry 
 0926:10  Landed 130 km E of Dzezkazgan

May 13,2026

  https://planet4589.org/space/jsr/back/news.855.txt