Friday, May 24, 1996

Kosmos 1773

 1986-064A



Kosmos-1773 
 

DateTimeEventOrbit  

1986 Aug 27  1140 Launch by Soyuz  KB  
 1148  Blok-I sep 
1986 Aug 27    (64B) 176x329x64.9, d Sep 2 
1986 Aug 27    89.66 173 x 341 x 64.9 
1986 Sep 4    89.32 170 x 310 x 64.9 
1986 Sep 10 
89.77 174 x 352 x 64.9 
1986 Sep 15    89.18 167 x 300 x 64.9 
1986 Sep 15   SpK-1 fiducial 
 0609?  Deorbit 
 0619?  Entry 
 0631?  Landed
1986 Sep 16   
90.00 173 x 374 x 64.9 
1986 Oct 1    88.73 162 x 260 x 64.9 
1986 Oct 2   
90.01 188 x 360 x 64.9 
1986 Oct 5   SpK-2 fiducial  
 0005? Deorbit 
 0015? Entry 
 0027? Landed
1986 Oct 18    89.41 183 x 307 x 64.9 
1986 Oct 18   
89.07 184 x 273 x 64.9 
1986 Oct 20  
 88.96 181 x 264 x 64.9 
1986 Oct 22  
 0300?  Deorbit 
 0312?  Entry 
 0326?  Landed

Thursday, May 23, 1996

Syncom 2

 1963-031A


The second Syncom payload, A-26 or Syncom B,was similar to the first. Launch was at 1433 UT on 1963 Jul 26. The apogee motor was successfully fired over 22S 39E (SAO-SR156) at 2005.01 UT on Jul 26, leaving Syncom II drifting 7 deg East per day. A burn at 2010 UT on Jul 27 reversed the drift to 4.5 deg West per day. By Aug 12, the drift was only 1.2 deg W/d, and at Aug 15 geosynchronous orbit was achieved with a mean longitude of 55 deg W, and an orbit of 35780 x 35865 km x 32.4 deg. Stationkeeping maneuvers were carried out on 1964 Mar 15 and 1965 Aug 19. By 1965 Jan the satellite had been moved to 73 deg East and was on loan to the US Department of Defense. By February, the stationkeeping propellant was depleted and Syncom II was drifting in longitude but otherwise operational. In 1965 Apr responsibility for Syncom II was transferred to DoD; the transfer was completed by 1965 Jul 8, with DCA in charge of the satellites and AFSCF controlling. The satellite was still working in 1966.


Syncom 2 
 

DateTimeEventOrbit  

1963 Jul 26  1433:00 Launch by Thor Delta 
 1435 Thor MECO 
 1435 Delta S/N 20006 burn 
 1436 T+3:30 St 3 spinup 
 1437? Delta SECO 
 1439? Altair burn 
 1439:51 T+6:51 Altair burnout 
 1443? Altair sep  230? x 36224 x 33.1 
 2005:56 AKM burn 20s 
 2006:16 AKM burnout 
1963 Jul 27  1910  Reverse drift  4.5W/d 
1963 Jul 31  2040  Axis correction 6.8W/d 
1963 Aug 11  1600  H2O2 burn, 14 min 
1963 Aug 12  0545  N2 Braking, 30min  1.2W/d 
1963 Aug 15  0520  N2 braking 46min 
1963 Aug 15   On station  35780 x 35865 x 32.4 GEO 55W 
1963 Aug 16  1544  East drift burn 2 min GEO 55W 
1963 Nov 28  0100 Resync burn  GEO 59W 
1963 Dec 2 Resume drift 
1963 Dec 10  1944   1436.21 35784 x 35793 x 32.9 GEO 59.1W+0.03E 
1964 Feb 11    1436.54 35789 x 35802 x 32.9 GEO 62.1W+0.1E 
1964 Mar 17   Stationkeep burn 3m/s  1.3W/d 
1964 Mar 19  1342   1435.41 35587 x 35958 x 33.4 GEO 68.1W+0.17W 
1964 Apr 19    1441.46 35891 x 35891 x 32.7 GEO 113.6W+1.3E 
1964 Apr 24   Braking, 0.8W/d 2m/s 
1965 Jan   Moved from Brazil to Indian Ocean  GEO 68E 
1965 Jan    GEO 73E 
1965 Jan 14    1438.55 35803 x 35865 x 32.2 GEO 174W+0.6E 
1965 Jun 1   Mv in  1436.05 35760 x 35811 x 31.8 GEO 26.2E+0.0W 
1965 Jul 8   To DoD 
1965 Aug 19   Stationkeep burn 
1965 Sep 24    1436.37 35759 x 35810 x 31.8 GEO 29.1E+0.0W 
1966 Feb 16    1435.74 35739 x 35819 x 31.2 GEO 69.4E+0.1W 
1968 Nov 14    1436.24 35762 x 35816 x 30.0 GEO 85.6E+0.04E 

Sunday, May 19, 1996

Club Management: September-October 1995

 https://welib.org/md5/00387231ea6ed85d040e01f22d7a2ed5

OSO 8

  1975-057A


Orbiting Solar Observatory 8 was a new type of OSO satellite. It was built by Hughes (and designated by them the HS-331 type satellite). OSO 8 was launched at 1143 on 1975 Jun 21 by a Delta 1910 from Cape Canaveral. The Delta second stage separated at 1218 leaving OSO 8 in a 95.5 min, 544 x 560 km x 32.9 deg orbit. OSO 8 transmitted until 1978 Sep 30. It reentered on 1986 Jul 9, the final recorded orbit being 153 x 161 km x 32.9 deg.


OSO 8 
 

DateTimeEventOrbit  

1975 Jun 21  1143:00  Launch by Delta 1910 
  SRM sep 
 1147:28  T+4:28 MECO 
  T+4:36 Stage 1 sep 
 1147:41 T+4:41 SES-1 4:59 
 1152:40 T+9:40 SECO-1 367 km 7.649 km/s  270? x 555 
 1208:46 T+25:46 SES-2 7s 483 km 7.499 km/s 
 1208:53  SECO-2 
 1216:22  OSO inertia booms deploy 
 1217:22? Spinup stage 2 
 1218  St 2 sep  95.5 544 x 560 x 32.9 
1978 Sep 30   end of tx 
1986 Jul 9   Reentered  

Aviation Week: April 1,1996

 https://welib.org/md5/d9272feb4a9c4eeb254db39d268cf669

Kosmos 1443

 1983-013A


This was a systems test of the TKS. It docked with Salyut-7 from March to August, and then continued free flight with a test of the VA capsule recovery.


Kosmos-1443 
 

DateTimeEventOrbit  

1983 Mar 2  0937:08 Launch by Proton  KB 
 0946  Stage 3 sep 
1983 Mar 2   88.9 195x252x51.6 
1983 Mar 5    90.3 193x395x51.6 
1983 Mar 5    90.5 259x349x51.6 
1983 Mar 5    90.4 280x314x51.6 
1983 Mar 9    90.2 260x312x51.6 
1983 Mar 10 0920 Docked with Salyut 7 
1983 Aug 14 1404 Undocked from Salyut-7 
1983 Aug 14    90.9 313x326x51.6 
1983 Aug 16    91.1 314x346x51.6 
1983 Aug 18    91.2 325x348x51.6 
1983 Aug 22   Capsule ejected 
 0955?  Separation 
 0958?  Deorbit 
 1008?  BSO sep 
 1024? Entry 

1045VA landed 100 km SE Arkalyk 
1983 Aug 23    91.2 326x347x51.6 
1983 Sep 16    91.14 322 x 338 x 51.6 
1983 Sep 17 0135  Orbit lower to 91.4 288x336x51.6 
1983 Sep 19
 0400? Deorbit 
 0430?  Impact S Pacific

Aviation Week: January 22,1996

 https://welib.org/md5/7ce963b283c706e285cdb3ca74045f82

STS-41-B (Challenger)

  1984-011A


The STS-11 mission was the first to fly under a revised numbering system. It was renamed mission 41-B. In this new system of two digits and a letter, the first digit represented the US fiscal year, so 4 meant that the launch had been first scheduled for FY84, which ran from Oct 1983 to Sep 1984. The B meant it was the second such mission (41-A retrospectively applying to either STS-9 or the cancelled STS-10, according to different sources). The second digit was always 1, which indicated launch from KSC - 2 was reserved for Vandenberg launches, but these never occurred. The new system was used in all public affairs releases and in JSC documents, but the old system was retained in parallel by KSC and I will use both systems. The old system was finally reinstated after the loss of mission 51-L.

Mission 41-B was launched on 1984 Feb 3. Westar 6 was deployed successfully on Feb 3, but unfortunately when the PAM-D motor fired it ended up in the wrong orbit. Next up was the IRT balloon, to be used for rendezvous tests, but it disintegrated upon inflation, so Challenger carried out maneuvers to rendezvous with a phantom target instead. On Feb 6 Palapa B2 was deployed, but met the same fate as Westar 6. The next day the mission's luck improved as McCandless and Stewart donned their spacesuits and headed into the payload bay at 1225. At 1310 the MMU-3 was checked out and at 1330 MS2 began the first MMU free flight, maneuvering it around the bay. At around 1405 McCandless flew it out to 50 m from the Orbiter and then returned to the bay; then out to 100m and back. Next he tested docking the T-PAD docking device to SPAS-1 in the payload bay. After this, Stewart took over MMU 3 in a 65 min flight which included more SPAS docking practice, while McCandless mounted the RMS arm for test of space repair tasks. By 1710 they returned to the cabin, and the airlock was repressurized after 5 h 55 min.

The second EVA began at 1040 on Feb 9. RMS problems prevented deployment of the SPAS target. EVA-2 saw McCandless fly the MMU-2 and carry out SPAS docking tests with the SPAS still latched in the bay. Then Stewart took out MMU-3 for a spin around the payload bay. Finally, Stewart carried out a Landsat refuelling simulation. The astronauts returned to the cabin at 1630 and the airlock was repressurized after 6h17m. 

On Feb 11, Challenger was the first orbiter to land at the Shuttle Landing Facility.


STS 41-B 
 

DateTimeEventOrbit  

1983 Sep 11    OPF/1 
1984 Jan 6    VAB/3 
1984 Jan 12    LC39A 
1984 Feb 3  1300:00  Launch  LC39A 
 1302:08  SRB sep, 46.5 km 
 1308:41  MECO, 110.0 km 
 1309:00  ET sep, 111.6 km  86.02 4 x 148 x 28.5 (dV) 
   86.02 -5 x 159 x 28.5 (dV) 
 1310:42  OMS 1 (2:30) 75.2m/s  95 x 306 
 1313:12  OMS 1 CO 
   88.55 100 x 304 x 28.47 (dV) 
 1324  ET apogee 
 1345:25  OMS 2 (2:05) 62.2m/s 
 1347:29  OMS 2 CO 
 1347  ET-10 breakup 
 1430  PLBD open  90.69 304 x 312 x 28.47 
 2059:23  Westar 6 deploy 
 2113:53  OMS 3 sep (RH 14s) 3m/s 90.80 306 x 321 x 28.5 
1984 Feb 5  0026  Mass 102719 
1984 Feb 5  0844   90.80 304 x 322 x 28.5 
 1023:23 OMS 4 (LH 31s) 8m/s  90.66 296 x 317? x 28.5 
1984 Feb 6  1108:32 OMS 5, rv test (LH 42s) 11m/s 90.27 279 x 296 x 28.5 
 1151  IRT deploy (disintegrated)  

 

1459   90.24 276 x 295 x 28.5 
 1513:16  Palapa B2 deploy 
 1528:16  OMS 6 sep (LH 12s) 3m/s 
 1625  RCS, rendezvous practice 
1984 Feb 7  0830   90.26 278 x 296 x 28.5 
 1202  Begin depress 
 1210  EVA-1 to BP at 5psi (MR) 
 1216  At 1psi 
 1217? Depress 
 1222? HO 
1984 Feb 7  1225  EVA-1 egress (AWST) 
 1225  Egress? 
 1230? MS2 checking out MMU3 
 1235?  MS2 begin MMU3 ops if flight is really 1:55 
 1310?  MS2/MMU3 flight 1:55 
 1318  MS2 flying MMU3 
 1330  Begin translation out 
 1335  Out to 50m 
 1355?  At 97m 
 1400  Stewart working with MFR 
 1405  Back near the FSS 
 1410  Stewart working with TPAD 
 1430  McC doffing MMU - end of MMU3 flight? 
 1435 Recharging N2 on MMU 
 1440? Stewart working on RMS/MFR 
 1452  Stewart preparing for MMU 
 1510?  65min MMU3/Stewart 1:09 
 1522  MMU3 around 20m 
  Break at 45 m 
 1528  MMU3 at 92m 
 1609  MMU3 work at TPAD/SPAS 
 1619? Stewart docking MMU3, end of flt 
 1631  Disconnecting TPAD from MMU 
 1646  Stewart working at MMU 
 1650  McC stowing at SESA 
 1720? Retrieve bay camera D 
 1749  Preparing for ingress 
 1752  HC 
 1755? Repress 
  Repress 5psi 5:55 
 1805  EVA-1 end (MR) 5:55 5 psi 
 1811  In airlock, working SCU power 
 1959   90.21 275 x 293 x 28.5 
1984 Feb 8   SPAS in-bay activities 
1984 Feb 9  0909  RMS unberthed 
1984 Feb 9  0923  RMS wrist joint failure 
 1007  RMS cradled 
 1020  Airlock at 5 psi 
1984 Feb 9  1024  EVA-2 depress (EVA begin, MR) - 5psi, on batt 
 1032? Vac 
 1036  HO  
1984 Feb 9  1040  EVA-2 begin 
 1040 McC egress 
  Stewart egress 
 1047  McC repairing slidewire 
 1058  Camera delta reinstalled 
 1137  Checking out MMU 2 
 1140?  (guess) MMU 2/McC flight 47 min 
 1227? MMU2 flight end 
 1245? MMU 2/St flight 44 min 
 1330? Exit MMU 
 1335?  Foot restraint came free during SPAS repair test 
 1340? EV-1 McCandless recovered and tethered foot restraint 
 1430? MMU 3/McC flight 1:08 
 1446? Stewart hydrazine transfer test 
 1538? MMU3 flight over 
 1624? Ingress Stewart 
 1628? Ingress McC 
 1630? HC 
 1635  Repressing  
 1641  EVA-2 end (MR) 6:17 
 1641  SCU power 5 psi 
1984 Feb 10  0830s  RCS DTO burn  
1984 Feb 10  0918   90.16 270 x 293 x 28.6 
1984 Feb 11  0800?  PLBD closed  90.16 269 x 294 x 28.6 
1984 Feb 11  1116:15 OMS DO (168s) 96.3m/s 
 1119:03  OMS DO CO 
 1145:12  Entry 
 1215:55  Landed  RW15 KSC 
 1216:06  NGTD 
 1216:59  Wheels stop 

Spaceflight: December 1995

 https://welib.org/md5/f357982d2c0fe8aad0193e3fcfb2479f

May 13,2026

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