Friday, July 26, 2002

SBS-2

 1981-096A


The second Satellite Business Systems spacecraft, SBS 2, was launched by Delta in Sep 1981 and stationed at 97W, three degrees from SBS 1. After being owned by MCI from 1985 to 1987, it was bought by Comsat. In 1983 it moved to 104W temporarily (from Jan to Mar). In 1988 the satellite moved to 99W, and back to 97W in late 1990. In Jan 1994 SBS 2 started a slow drift to 71W, arriving in October.


SBS 2 
 

DateTimeEventOrbit  

1981 Sep 24  2309  Launch by Delta 3910-Pam D  CC LC17 
  SRM 1-5 burn 
  T+0:57 SRM 1-5 off 
  T+1:04 SRM 1-5 sep 
  T+1:04 SRM 6-9 on 
  T+2:00 SRM 6-9 off 
  T+2:07 SRM 6-9 sep 
  T+3:43 St 1 MECO 
  T+3:51 St 1 sep 
 2312 T+3:57 SES-1 5:06 
 2313 Fairing sep
 2318 T+9:03 SECO-1 suborbital  -781? x 282? x 28.5 
 2329 T+20:14 St 2 sep 
 2329 T+20:52 TES 86s 
1981 Sep 24  2331  T+22:18 TECO PAM-D burnout 
1981 Sep 24  2333  T+24:26 PAM-D separation  650.62 165 x 36822 x 27.7 
1981 Sep 25  0500?  Apo 1 87E 
 1600? Apo 2 77W 
1981 Sep 26  0200? Apo 3 127E 
 1300? Apo 4 37W 
 2300? Apo 5 167E 
1981 Sep 26  2257  AKM  1401.62 34287 x 35930 x 0.3 GEO 171.5E+8.8E 
1981 Sep 28  1420  Despin 
1981 Sep 28  2135  Solar panel deploy 
1981 Sep 29   Transfer from COMSAT to SBS 
1981 Sep 30    1424.56 35495 x 35623 x 0.3 GEO 176.4W+2.9E 
1981 Oct 26    1424.37 35491 x 35621 x 0.2 GEO 100.2W+3.0E 
1981 Nov   mv in 
1981 Nov 5    1436.12 35773 x 35801 x 0.2 GEO 96.7W 
1982 Jan 2    1436.04 35773 x 35797 x 0.1 GEO 96.9W 
1983 Jan 21    1436.12 35786 x 35787 x 0.0 GEO 97.0W 
1983 Jan   Move to 104W 
1983 Jan 27    1436.16 35770 x 35805 x 0.1 GEO 104.5W 
1983 Mar 2    1436.10 35780 x 35793 x 0.0 GEO 104.5W 
1983 Mar   move to 97W 
1983 Mar 11    1436.10 35784 x 35788 x 0.0 GEO 97.0W 
1984 Nov 15    1436.12 35783 x 35790 x 0.1 GEO 97.0W 
1987 Jan 3    1436.12 35785 x 35788 x 0.0 GEO 97.1W 
1988 Aug 6   mv out  1436.15 35776 x 35799 x 0.5 GEO 97.2W+0.02W 
1988 Oct 11    1436.23 35777 x 35800 x 0.6 GEO 98.8W+0.04W 
1988 Oct 28   mv in  1436.15 35775 x 35800 x 0.7 GEO 99.3W 
1989 Jul 2    1436.09 35780 x 35792 x 1.4 GEO 99.1W 
1990 Sep 24    1436.07 35774 x 35798 x 2.4 GEO 99.1W 
1990 Nov 26    1436.00 35772 x 35796 x 2.6 GEO 98.5W 
1990 Nov   move to 97W 
1991 Jan 23    1436.05 35773 x 35797 x 2.7 GEO 97.1W 
1991 Apr 28    1436.11 35774 x 35799 x 3.0 GEO 97.0W 
1993 Jun 7    1436.12 35771 x 35802 x 4.8 GEO 97.0W 
1994 Jan 25    1436.10 35735 x 35838 x 5.3 GEO 97.0W 
1994 Jan 27   mv out  1435.09 35752 x 35781 x 5.3 GEO 96.5+0.2E 
1994 Jun 9   mv in  1435.67 35767 x 35789 x 5.6 GEO 73.7W+0.1E 
1994 Jul 16    1435.85 35772 x 35791 x 5.6 GEO 70.6W 
1994 Oct 22    1436.36 35778 x 35804 x 5.8 GEO 71.1W+0.07W 
1994 Oct 24   mv in  1436.08 35722 x 35850 x 5.9 GEO 70.8W 
1994 Oct 30    1436.08 35719 x 35853 x 5.9 GEO 70.8W 
1995 Nov 7    1436.07 35780 x 35792 x 6.6 GEO 70.9W 
1996 May 7    1436.16 35782 x 35793 x 6.9 GEO 71.0W 
1996 Aug 28    1436.15 35781 x 35794 x 7.1 GEO 71.0W 
1996 Sep 7   mv out  1438.11 35811 x 35840 x 7.1 GEO 72.3W+0.5W 
1997 Apr 5    1437.72 35801 x 35835 x 7.5 

STS-82 (Discovery)

 1997-004A


Discovery was launched in Feb 1997 on the second HST Servicing Mission. Reaching almost 600 km in altitude, OV-103 closed in on Hubble over a couple of days. Steve Hawley, who had released the observatory using RMS 301 on Discovery in 1990, captured the satellite with the same RMS arm on Feb 13. Hawley quickly installed HST on its mounting point on the Flight Support System in the aft cargo bay.

On Feb 14 Mark Lee and Steven Smith entered the external airlock for the first EVA. This was the first time an ODS airlock had been carried at the front of the cargo bay and the first time a spacewalk was made from the ODS hatch. The ODS has two hatches, one on top used to go through the docking system, and one at the rear which on Mir missions leads to the Spacehab module. The rear hatch was used on this mission.

As the ODS was depressurized from 10 psi to 5, the +V2 solar array on HST was observed to suddenly slew 40 degrees. It was later realized that escaping air from the airlock had hit the panel; a density spike on the FOS instrument was recorded at the same time. The airlock was held at 5 psi while the situation was discussed. One orbit later the depress was resumed; the astronauts had been ahead of schedule so the delay was not serious.

Once in the payload bay, Lee and Smith spent some time setting up equipment, and then removed the GHRS instrument from Hubble's aft compartment, replacing it with the new STIS imaging spectrograph. GHRS was stowed in STIS's container on the ORUC Spacelab pallet. Next, the NICMOS infrared camera/spectrograph, carried up in the SAC carrier, replaced the old FOS ultraviolet spectrograph, giving HST an infrared capability for the first time.

The second EVA, on Feb 15, featured installation of the replacement Fine Guidance Sensor used to guide HST accurately. A tape recorder, ESTR-2, was also replaced in equipment bay 8. EV crew member Tanner used Smith's spacesuit, the first time such sharing had been done (leg and arm components had to be switched).

The third EVA was on Feb 16. After depress, hatch opening was delayed briefly while problems with Lee's suit were resolved. The astronauts entered the bay; this time Lee went on the RMS. He removed a DIU interface box and replaced it. Then Smith came onto the RMS and installed a new solid state data recorder in equipment bay 5. Finally, a reaction wheel gyro assembly was replaced. The astronauts inspected damaged multi-layer insulation (MLI) and found that it could not be easily repaired with Kapton tape. The orbit was again raised.

The fourth EVA saw replacement of solar array drive electronics, add protective covers over the magnetometers near Hubble's aperture, and install MLI blankets on damaged areas at the aperture end. The spacewalkers were Harbaugh and Tanner.

The fifth and final EVA was devoted to further repairs on the insulation. Lee and Smith completed the job in two and a half hours, but then HST engineers noticed a possible problem in a reaction wheel assembly which could have required the astronauts to replace it. The spacewalkers were told to return to the airlock and remain there while the problem was analysed. Eventually it was decided not to decide that day, retaining the option for a spacewalk the following day (an option which was not used). Lee and Smith returned to the payload bay briefly to stow the Manipulator Foot Restraint which had spent the week attached to the remote manipulator system, and complete their payload bay cleanup; they then went back to the airlock and repressurized, completing the repair activities for the mission. A final orbital reboost soon followed.


STS-82 
 

DateTimeEventOrbit  

1997 Feb 11  0855:17  Launch STS-82  KSC LC39A 
 0857:20  SRB sep 
 0903:46  MECO 
 0903:56  ET sep  57 x 572 x 28.5 
 0939:50  OMS-2 2:52 83.9m/s 350 x 579 x 28.5 
 0942:43  OMS-2 CO 
 1015?  PLBD checkout partial open/close 
 1037  PLBD open 
 1422:34  OMS-3 1:14 36 m/s  480 x 579 x 28.5 
 1423:48  OMS 3 CO 
1997 Feb 12   RMS checkout 
 1231:38  OMS-4 NSR 56s 29m/s  576 x 584 x 28.5 
 1232:35  OMS 4 CO 
 1357:17  NC2 RCS 13s 1m/s 
1997 Feb 13  0201:21 OMS-5 NH burn 8s 4m/s 
 0201:03  OMS-5 CO 
 0248:17  NC3 burn RCS 1m/s 14s 96.51 589 x 593 x 28.5  
 0355:41  NPC-2 RCS 0.2m/s 2s 
 0503:03  NCC RCS 0.4m/s 1s 
 0524  RMS power up 
 0528  Range to HST 20 km 
 0531  RMS uncradle 
 0603:09  TI burn, 1m/s 12s mass = 105917 kg  96.57 589 x 598 x 28.5 
 0629  MCC 1 
 0658  MCC 2 6s, 6 km range 
 0707  MCC 3, 3s 
 0717  MCC 4, 1.2 km range 
 0722  On HST -R-bar  589 x 598 x 28.5 
 0833:53  RMS grapple HST 
 0904 Berthed and latched on FSS 
 0912:13  Berthing complete 
 0914 RMS ungrapple 
 0920  RMS survey of HST  96.57 589 x 598 x 28.5 
  RMS extended park position 
1997 Feb 14   EVA-1  
 0244  Airlock in depress to 5 psi 
 0245 HST Solar array moves due to depress air; EVA postponed. 
 0415 Resume depress 
 0429  Depressurized, EVA begins (JCM)  96.56 590 x 597 x 28.5 
 0429:53  AL depress complete (NASA) 
 0434  EVA begins (NASA)  
 0435  Slew +V2 array back to horizontal 
 0440? Hatch open; Lee egress  
 0445  Smith egress to bay 
 0454  RMS grapple MFR 
 0507  Smith on RMS 
 0548  Open HST compartment 
 0619  GHRS removed from HST 
 0633  GHRS parked on ORUC 
 0640  STIS removed from ORUC SIPE 
 0724  STIS installed in HST 
 0750  GHRS placed in ORUC SIPE 
 0810? FOS removed from HST 
 0826  FOS parked on ORUC 
 0830  NICMOS removed from SAC SIPE 
 0900  NICMOS installed in HST 
  Install cryo vent line on NICMOS 
 0940  HST aft shroud closed 
 1016  HST aft shroud latched 
 1050  FOS placed in SAC SIPE 
 1116  Hatch closed  
 1116:32  Repress 
1997 Feb 15   EVA-2 Harbaugh, Tanner 
 0250  Begin depress 
 0321  EVA depress (JCM) 
 0323:11  AL depress complete (MR) 
 0325  EVA begins (NASA) 
 0332  Egress  
 0400  Tanner on RMS 
 0500  FGS-1 removed 
 0510  FGS-1 on ORUC fixture 
 0522  FGS-1R removed from FSIPE 
 0541  FGS-1R installed 
 0650  FGS-1 in FSIPE 
  ESTR-2 removed 
 0740  ESTR-2R removed from contained 
 0800  ESTR-2R installed 
  Survey of solar array damage 
 0850  Harbaugh on RMS 
 0900  OCE-EK installation, Bay C 
  Orbit raise 22 min 
 1044  Hatch closed 
 1051  End of EVA (NASA) 7:26 
 1053:01  Repress, end of EVA 7:30 
 1502:19  VRCS reboost, avoid 94-029 debris. 10 min 
1997 Feb 16   EVA-3 Lee, Smith 
 0250:56 AL depress complete 
 0251? Depress  
 0253  EVA begins (NASA)  96.56 589 x 597 x 28.5  
  Lee on RMS 
 0430  DIU removed 
 0550  new DIU installed 
 0640?  SSR work 
 0745?  SSR installed 
 0800?  RWA installed 
 0850?  RWA complete 
  MLI damage inspection  
  Hatch closed 
 1003:37  Repress 7:13  
 1010:16 VRCS reboost 2  
 1030:03 RCS complete 
 1200   86.76 597 x 608 x 28.5 
1997 Feb 17  0340  EVA-4 Harbaugh, Tanner 
 0343:24  Depress complete  
 0345  EVA start, NASA 
 0351  Hatch open 
 0410  Harbaugh on RMS 
 0420  begin SADE repair 
 0645  Done SADE repair 
 0757  MSS cover repair complete 
 0805  Begin insulation repairs at top of HST 
 0920  Insulation repairs complete 
 0937  Harbaugh off RMS 
 1014  Hatch closed  96.75 597 x 608 x 28.5 
 1019:32  Repress, end of EVA  
1997 Feb 18   EVA-5 Lee, Smith 
 0305  Depress  96.75 597 x 608 x 28.5 
 0312:42  Depress complete (MR) 
 0315  NASA EVA start 
 0320  Hatch open 
 0330  Lee on RMS 
 0336  MLI insulation repairs 
 0545  Repairs complete 
 0627  Ingress, hatch closed 
 0733  Hatch open, egress 
 0749  Remove MFR from RMS 
 0823  Ingress, Thermal cover closed 
 0827  Hatch closed 
 0829  O2 to press 
 0831:28  Repress 
 1028  Reboost VRCS 32 min 
 1100  Reboost-3 complete 
 1245   96.88 598 x 619 x 28.5 
1997 Feb 19  0321:09  RMS grapple HST  
 0502:56  RMS unberth HST 
 0557  Open HST aperture door 
 0641:21  Release HST 
 0642:06 SEP1 0.4m/s 5s 
 0717  SEP2, 0.4m/s 5s 300m range 
 0758  SEP-2A 0.4m/s 5s 
 1059   96.86 598 x 618 x 28.5 
 2200   96.86 598 x 617 x 28.5 
1997 Feb 20  0841  RCS perigee lower, 4m/s 52s  96.70 583 x 617 x 28.5 
1997 Feb 21  0308  Close PLBD  
 0721:54  OMS DO 4:59 153.8m/s  52 x 611 x 28.5 
 0726:53 OMS cutoff  57 x 616 x 28.5 (TLE) 
 0801  Entry interface 122 km  
 0832:26 Landed RW15 KSC 
 0832:37  NGTD 
 0833:24Wheels stop 

Sunday, July 21, 2002

Himawari 1

 1977-065A


NASDA and the JMA (Japanese Meteorological Agency) developed the Geostationary Meteorological Satellite (GMS) program as part of an international weather watch initiative. The first GMS, named Himawari (Sunflower) after launch, was built by Hughes using the HS-335 bus with collaboration by Nippon Electric.


Himawari 
 

DateTimeEventOrbit  

1977 Jul 14  1039  Launch by Delta 2914  CC LC17 
  T+0:38 SRM 1-6 off 
  T+0:39 SRM 7-9 on 
  T+1:17 SRM 7-9 off 
  T+1:27 SRM 1-9 sep  -6300 x 30 ? 
  T+3:48 MECO 
  T+3:56 St 1 sep 98 km  -4000 x 200 ? 
  T+4:01 SES-1 
 1043 T+4:45 Fairing 
 1048  T+8:57 Delta SECO-1  174 x 174 x 27.2 
 1100  T+21:17 SES-2 
 1100  T+21:24 SECO-2  172 x 565? x 27.2  
 1101 T+22:14 spinup 
 1101 T+22:16 St 2 sep   
 1101 T+22:58 TES 
 1102 T+23:42 TECO 
 1103 T+24:55 Star 37 sep  174 x 36655 x 27.2 (PK) 
  Delta depletion burn  263 x 600 x 28.7 (65C) 
  Delta depletion burn  522 x 1997 x 29.1 (65B) 
 1612 Delta explosion 
 1700? Apo 1 
1977 Jul 15  0330? Apo 2 
1977 Jul 15  1400? Star 27 burn, apo 3  
  Star 27 sep 
   GEO 140E 
1977 Jul 18    1436.48 35775 x 35812 x 1.2 GEO 140.3E+0.1W 
1977 Aug 28    1436.09 35770 x 35803 x 1.1 GEO 140.1E 
1981 May 10    1436.13 35780 x 35793 x 1.0 GEO 140.2E 
1981 Dec 15   Mv out 
1982 Jan 25   On station, standby GMS  GEO 160E 
1982 Jan 25    1436.10 35781 x 35792 x 0.8 GEO 160.4E 
1983 Dec 23    1436.14 35784 x 35790 x 2.4 GEO 160.2E 
1984 Jan?   Move to prime position 
1984 Feb 15    1436.00 35775 x 35794 x 2.5 GEO 140.0E 
1984 Aug 3    1436.20 35784 x 35792 x 2.9 GEO 139.9E 
1984 Aug 5   mv out 1433.88 35697 x 35789 x 2.9 GEO 140.9E+0.5E 
1984 Sep 11   mv in  1436.18 35780 x 35796 x 3.0 GEO 160.0E 
1986 Oct    GEO 159.5 E 
1987 Jan 2    1436.15 35781 x 35793 x 5.1 GEO 159.5E 
1989 Jun 23    1436.19 35782 x 35794 x 7.3 GEO 159.2E 
1989 Aug 16   mv out 1435.52 35716 x 35833 x 8.1 GEO 135.4E+0.14E 
1989 Sep 17   orbit raise 1450.90 36007 x 36144 x 7.6  
1995 Oct 22    1450.88 36021 x 36130 x 12.2  
1999 Apr 20    1450.91 36011 x 36140 x 13.7 

Kosmos 1438

 1983-005A


Two-tone telemetry; Hi res satellite


Kosmos-1438 
 

DateTimeEventOrbit  

1983 Jan 27  0830 Launch by Soyuz-U  Baikonur 
 0834 Blok-I burn 
 0838  Blok-I sep 
1983 Jan 27   88.89 209x230x70.4 
1983 Jan 28    89.65 167x346x70.4 
1983 Feb 1  89.97 190x356x70.4 from 89.54 166x337 
1983 Feb 2    89.97 210x335x70.4 
1983 Feb 4    89.22 205x266x70.4 
1983 Feb 6  89.17 205x261x70.4 
1983 Feb 7   
 0520?  Deorbit 
 0530? PO sep 
 0539? Entry 
 0553? Landed 

Saturday, July 20, 2002

Seventeen: March 2002

 https://welib.org/md5/b34cfe856e1fecde65afae252177dd8d

Soyuz TM-3

 1987-063A


The third 7K-STM/Soyuz TM, 11F732 No. 53 (Soyuz TM-3) was launched in Jul 1987.


    Crew

  • Komandir Podpol. Aleksandr Viktorenko, VVS

  • Bortinzhener Aleksandr Aleksandrov, NPO Energiya

  • Kosmonavt-issledovatel' Lt-Col. Muhammad al Faris, Syrian AF.


Soyuz TM-3, Flight 1 
 

DateTimeEventOrbit  

1987 Jul 22  0159  Launch by Soyuz-U2  KB  
 0201 Blok-BVGD sep 
 0203  Blok-A sep  
 0207  Blok-I cutoff 
 0207  Blok-I sep 
  
88.63 193 x 217 x 51.62 
 0930   89.84 236 x 298 x 51.6 
1987 Jul 23    89.78 230 x 297 x 51.6 
 1900   89.83 234 x 298 x 51.6 
1987 Jul 24  0230   91.23 302 x 367 x 51.6 
 0331  Docked with Mir 37KE +X 

A week later, Romanenko and Aleksandrov moved the Soyuz to the front port.


    Crew

  • Komandir Pol. Yuriy Romanenko, VVS

  • Bortinzhener Aleksandr Aleksandrov, NPO Energiya


Soyuz TM-3, Flight 2 
 

DateTimeEventOrbit  

1987 Jul 30  2155Crew entry 
 2328  Undocked from Mir 37KE +X 
 2348  Redocked at Mir -X 

Soyuz TM-3 returned from Earth on Dec 29.


    Crew

  • Komandir Pol. Yuriy Romanenko, VVS

  • Bortinzhener Aleksandr Aleksandrov, NPO Energiya

  • Kosmonavt-issledovatel' Anatoliy Levchenko, Min. Av.


Soyuz TM-3, Flight 3 
 

DateTimeEventOrbit  

1987 Dec 29  0555  Undocked from Mir -X  
 0700? BO sep 
 0823  Deorbit 
 0827? DO CO 
 0850? PAO sep 
 0855? Entry 
 0916  Landed 80 km NE of Arkalyk 

Sunday, July 14, 2002

Garuda 1

 2000-011A


PT Asia Cellular Satellites / ACES Asia Cellular Satellite System for hand held and mobile telephone service to Asia, 1999 early 12-m dia L-band antennas proposed by Lockheed Martin/Bethesda. Contract to LM/Bethesda SN950710-2 for two A2100AXX L-band satellite. Launch by Proton / DM3. Payload integration at Newton, Pennsylvania; spacecraft integration at Sunnyvale. In 1999 LM-GT invested in ACES and the ACES company relocated from Jakarta to Bermuda.


Garuda 1 
 

DateTimeEventOrbit  

2000 Feb 12  0910:54  Launch by Proton  KB PL81 PU23 
  T+02:02 Stage 2 burn 
  T+02:03 RK-1 Stage 1 sep 
  T+05:30 St 2 MECO 
  T+05:31 RK-2 Stage 2 sep 
  T+05:40 Stage 3 burn 
  T+05:42 GO sep
  T+09:38 GK St 3 MECO  
 0920:37 T+09:43 St 3 VECO 
  T+09:43 Stage 3 sep, 7.28km/s 79.80 -630 x 168 x 51.61 
 0920:38 T+9:44 SOZ 
 0921:32 T+10:38 DM adapter sep 
 0926:39  T+00:15:45 DM burn 1 69s 
 0927:45  T+00:16:51 DM MECO-1  170 x 170 x 51.6 
 1024:03  T+01:13:09 DM MES-2 
 1030  T+01:20:27 DM MECO-2  170 x 36000 x 51.5 
 1527  T+06:17:48 DM MES-3 
  T+6:17:49 SOZ sep 
 1529  T+6:19:51 DM MECO-3 
 1550:44  T+6:39:51 Blok DM 15L sep  6233 x 35946 x 16.0 
  T+8:24:51 Depletion 
 1739  T+8:29:51 Depletion MECO 
2000 Feb 14   LAM-1  805.17 8589 x 35993 x 14.0 
2000 Feb 16   LAM-2  907.93 13667 x 35995 x 10.2 
2000 Feb 18   LAM-3907.20 13337 x 35992 x 10.2 
2000 Feb 19  1500?  LAM-4 
2000 Feb 21    1389.13 33731 x 35993 x 3.4 
2000 Feb 22  1300?  LAM-5 
2000 Feb 22    1441.62 35787 x 36001 x 3.0 GEO 127.5E+1.3E 
2000 Feb 24   Antenna deploy 
2000 Feb 25    1438.81 35772 x 35907 x 3.0 GEO 123E 
2000 Mar 1    1436.12 35775 x 35798 x 3.0 GEO 122.9E 
2000 May 23    1436.23 35769 x 35809 x 2.8 GEO 122.6E 

Kosmos 1381

 1982-062A


Two-tone telemetry; Medium res satellite


Kosmos-1381 
 

DateTimeEventOrbit  

1982 Jun 18  1300 Launch by Soyuz-U  Baikonur 
 1304 Blok-I burn 
 1308  Blok-I sep 
1982 Jun 18    90.33 203x379x70.4 
1982 Jun 19    92.71 378x437x70.4 
1982 Jun 21    92.71 363x452x70.4 
1982 Jun 26    92.54 362x437x70.4 from 92.71 364x451 
1982 Jun 30   92.56 363x438x70.4 
1982 Jul 1  
 0906? Deorbit 
 0916? PO sep 
 0935? Entry 
 0947? Landed 


Monday, July 8, 2002

Transit T-2

  1975-099A


APL's Transit Improvement Program 2 satellite was launched in Oct 1975. The main experiment experienced issues due to problems with the solar panels but the experimental ion micro-thrusters were tested successfully.


TIP 2 
 

DateTimeEventOrbit  

1975 Oct 12  0639:36  Launch by Scout D-1  V SLC5 
  T+1:21 St 1 burnout  
  T+1:25 St 2 burn 
  T+2:04 St 2 burnout  
  T+2:15 Heatshield 
  T+2:17 St 3 burn  
  T+2:50 St 3 burnout 
  T+7:46 Spin motor  
  T+7:48 St 3 sep 
 0647?  T+7:53? St 4 burn  
 0648:03?  T+8:27? St 4 burnout 
 0648?  St 4 sep 
   95.3 362 x 705 x 90.7 
1975 Oct   Solar panels failed? 
1975 Dec 8    85.53 365 x 722 x 90.7 
1975 Dec 24    97.41 452 x 816 x 90.5  
1975 Dec 30    98.16 523 x 817 x 90.4 
1976 Mar 1    98.39 541 x 821 x 80.3 
1976 Mar 6    98.64 567 x 818 x 80.4 
1976 Mar 22   Orbit raise 98.85 585 x 821 x 90.4 
1976?   Decommissioned 
1991 May 26   Reentered 

Saturday, July 6, 2002

Soyuz TM-24

 1996-047A


EO-22 crew commander Gennady Manakov was pulled off the flight because of a heart problem only a week before launch, and he and prime flight engineer Pavel Vinogradov were replaced by the backups Valeriy Korzun and Aleksandr Kaleri. They joined cosmonaut-researcher Claudie Andre-Deshays of CNES. The CNES portion of the mission was codenamed Cassiop'ee.


Soyuz TM-24 
 

DateTimeEventOrbit  

1996 Aug 17  1317:52 Ignition 
 1318:03  Launch by 11A511U  KB  
 1320:03  Blok BVGD sep 
 1320:06  Escape tower sep 
 1320:43  Fairing sep 
 1322:48  Blok A cutoff 
 1322:51  Blok A sep 
 1323:03  Blok-I burn  
 1323:10  Interstage sep  
 1326:53  Blok-I cutoff 
 1327  Blok-I sep  
 1330Deploy rendezvous antennae 
 1334Deploy solar panels 
 1341Deploy comms antennae 
 1647:43 TCM1 
 1750:21  TCM2 
1996 Aug 19  1450:21 Docked -X Mir  

The second flight of the craft was a redocking from the front to the rear (+X) end of Mir. The crew were Korzun, Kaleri and Linenger.


Soyuz TM-24 flight 2 
 

DateTimeEventOrbit  

1997 Feb 7  1628:01  Undocked -X Mir 
 1651:27  Docked +X Kvant 

The crew of Korzun, Kaleri and Ewald undocked on Mar 2. The spaceship landed at 47 49 N 69 24 E in Kazakstan.


Soyuz TM-24 flight 3 
 

DateTimeEventOrbit  

1997 Mar 2  0324:57  Undocked  
 0329:30  Sep burn 
 0550:12  Deorbit 115.2m/s 
 0554 Deorbit complete 
 0614BO, PO sep 
 0617Entry 
 0644:15Landed 

These Are Not My Beautiful Stories

  Summary: The chapters within are outlines for both future stories I’ve got planned (in the case that I never get around to writing them) a...