Sunday, December 26, 1999

STEX

 1998-055A


The NRO's STEX Space Technology Experiment, built by LMA/Denver, is a satellite to test a space tether and a xenon electric propulsion system using TsNIIMash TAL-D55 Hall Effect thrusters, integrated by Primex. Eight P-59 (MR-103D) 1N hydrazine REMs are also used for propulsion. Size is 0.9 x 0.9 x 2.4m, mass is 700 kg; launch was by Taurus. The ATEX deck is 0.81 x 0.81 x 0.03m with a mass of 29 kg; STEX without the deck is 1.23 x 1.23 x 2.05m with a mass of 490 kg, plus two 0.5 x 2.0 x 1.7m, 10 kg solar panels. Total STEX dry mass is 539 kg.


STEX 
 

DateTimeEventOrbit  

1998 Oct 3  1004  Launch by ARPA Taurus  V 576E 
  Stage 0 sep 
 1005  T+0:56 Stage 1 burn  
 1006  T+2:21 Stage 1 sep 
 1006  T+2:23 Stage 2 burn 
 1006  T+2:26 Fairing sep 
  Stage 2 cutoff 
 1014  T+10:10 Stage 2 sep 
 1014  T+10:21 Stage 3 burn 
 1015  T+ 11:34 Stage 3 cutoff 
 1017  T+13:29 Stage 3 sep  98.32 671 x 700 x 85.07 (WWW) 
 1017  T+13:41 Stage 3 CAM (avoidance) 
  T+16:51 Stage 3 CAM complete   
  T+41:34 RCS depletion 
   98.8 695 x 713 x 85.0 (UN) 
1998 Oct 7   EPDM electrical testing 
1998 Oct 23   Hall Thruster burn 40mN, 1km raise 
  Orbit raising 
1998 Nov 13   At final orbit  744 x 757 x 85.0 
1999 Jan 16  2306  Begin ATEX deploy 
 2324:06  Tether off course 
1999 Jan 16  2324:17  ATEX separated at 21m deploy 

Soyuz TM-22

 1995-047A


Soyuz 7K-STM No. 71 (Soyuz TM-22) was launched on 1995 Sep 3 with the EO-20 crew Yuriy Gidzenko, Sergey Avdeev and Thomas Reiter (ESA). ESA referred to the mission as Euromir-95. Reiter's position was second flight engineer (Bortinzhener-2).


Soyuz TM-22 
 

DateTimeEventOrbit  

1995 Sep 3  0900:23  Launch by Soyuz 11A511U2  KB LC1 
 0909  Blok-I sep 
1995 Sep 3    88.65 197 x 217 x 51.6 
1995 Sep 3  1440   89.72 232 x 288x 51.6 
1995 Sep 4    89.75 237 x 286 x 51.7 
1995 Sep 5    89.74 237 x 266 x 51.6 
1995 Sep 5  1030  Docked with -X Mir 
1995 Sep 5    92.47 392 x 397 x 51.6 
 1225Hatch open 

Gidzenko, Avdeev and Reiter returned to Earth on 1996 Feb 29 after handing over the station to the EO-21 crew. The mission lasted 179d 01h 41m 45s.


Soyuz TM-22, Flight 2 
 

DateTimeEventOrbit  

1996 Feb 28    92.45 390 x 398 x 51.7 
1996 Feb 29  0720 Undocked 
 0945  Deorbit burn 
 0949  Deorbit cutoff 
 1012? Modules sep 
 1016?  Entry  0? x 396 x 51.6 
 1042:08 Landed 

Seventeen: May 1999

 https://welib.org/md5/92a64db2ca44c31d9c6df33c47a3f337

Saturday, December 25, 1999

STS-61 (Endeavour)

 1993-075A


The first HST Servicing Mission was launched on 1993 Dec 2. The astronauts reported tally-ho (visual sighting of the target) at 0746 on Dec 4.  The EVA-2 repress was halted at 0.8 psi for 4 minutes and depressurized again to clear KT's ears. A slow repress began at 6h45m into the EVA and by 1017 the pressure reached 4.5psi, 6h 52m into the EVA (the official EVA time was 6h36m). Cabin pressure was reached at 1022.


STS-61 
 

DateTimeEventOrbit  

1993 Oct 21   Tow to VAB  
1993 Oct 22   ET mate  VAB/1 
1993 Oct 28   Rollout  LC39A 
1993 Nov 15   Pad transfer  LC39B 
1993 Dec 2  0927:00  Launch  
 0929:06  SRB sep 
 0935:32  MECO  90.81 58 x 569 x 28.5 
 0935:51  ET sep 
 1010:30  OMS-2 3:21 99m/s 94.33 401 x 570 x 28.47 
 1013:51  OMS-2 CO 
 1057  PBD open 
 1454:28  NC1 (OMS-3 59s) 30m/s  95.40 504 x 570 x 28.5  
1993 Dec 3  0414   95.45 509 x 570 x 28.5 
 0927  RMS uncradle 
 1100  (HST ap. door closed) 
 1230  RMS cradle 
 1310:59  NSR (OMS-4 30s) 15m/s  559 x 572 x 28.5  
 1344:14  NC2 (OMS-5L 17s) 4m/s  561 x 587 x 28.5  
1993 Dec 4  0234  NH   
 0322:30  NC3 (OMS-6R 15s) 4m/s  96.39 579 x 592 x 28.5 
 0403:52  NPC (RCS 5s)   
 0532  Radar lock on HST 
 0535  NCC (RCS 12s)  
 0635:02  TI  
 0657  RMS uncradle 
 0715?  MCC-1 
 0729  MCC-2 (RCS 2s) 
 0738  MCC-3 (RCS 2s)  
 0749  MCC-4 (RCS 2s)  96.45 585 x 591 x 28.5  
 0753  HST to capture attitude 
 0755  Braking 
 0830  Range 30 m 
 0846:56  RMS grapple HST 
 0924:30  HST berthed on FSS/BAPS 
 0926  HST latched 
 0932  HST on umbilical 
 0935  RMS ungrapple HST 
 1000  HST on external power  96.45 585 x 592 x 28.5 
1993 Dec 5  0329  HST SA I slew horizontal 
 0329  EVA-1 begin depress 
 0335:20  Resume depress from 5psi 
 0338:40  Complete depress 
 0342:09  Hatch open 
 0344:26  EMU on battery power
 0351  Egress 
 0404  RMS grapple MFR 
 0410  EV-1 ingress MFR 
 0433  Opening HST for RSU work 
 0517  Replace first RSU 
 0541  Begin replacing second RSU 
 0554  Second RSU change complete 
 0610  Problems with HST bay door closing 
 0734  Replacing ECUs 
 1030  Completed ECU and door closing work 
 1113  SA I slew horizontal 
 1122  EV-1 egress MFR 
 1123  HST pivot/rotate 
 1128  EV-1 ingress 
 1130  HC  
 1138:24  Repress 08:00 (offl. 07:54) 
 1200   96.45 585 x 592 x 28.5 
 1325  SA-I first panel SDM retract 
1993 Dec 6  0325  EVA-2 depress 
 0328  HO 
 0329:02  EMU on bat 
 0347?  Thornton on MFR 
 0438  SA I released from HST,  
  held by Thornton 
 0451.15  SA I jettison by Thornton 
 0451  RCS sep 
 0515? SA II from SAC, transferred to HST  
 0530  SA II attached 
 0705  Preparing to separate SA I second wing 
 0730  SA I second wing unlatched 
 0744  old wing secured to carrier 
 0822  Preparing to latch new wing in place 
 0909  SA II second wing attached 
 0952  Thornton off MFR 

 

0958.53  HC 
 1004:32  Repress begins 
 1005  Repress halted at 0.8psi 
 1007  Depress 
 1009  At 0.3 psi 
 1009  repress 
 1016  At 4.5 psi 
 1023  At cabin pressure 
1993 Dec 7  0326  EVA-3 depress  
 0328  5psi leak check till 0330 
 0333  Depress complete 
 0333.41  HO 
 0335:44  EMU on bat 
 0343  Hoffman egress 
 0347  Hoffman on MFR 
 0347  Musgrave egress 
 0443  WFPC-1 removed 
 0520  WFPC-1 in temp fixture 
 0535?  WFPC-2 out of case 
 0605  WFPC-2 installed 
 0644  Cover on WFPC1 
 0657  Start putting WFPC1 into case 
 0712  WFPC1 secure in case 
 0725  Stowing PFRs 
 0748  BAPS tilting HST forward for MSS access 
 0803  Magnetometers on RMS 
 0834  First mag installed 
 0914  Second mag installed 
 0930  PLB cleanup 
 1003  Musgrave ingress 
 1010  Hoffmann egress MFR 
 1015  Hoffman ingress 
 1018  Hatch closed 
 1023:05  Repress 06:51 (off. 06:47) 
1993 Dec 8  0258  Depress to 5psi 
 0304  Depress resume, EVA-4 
  Thornton, Akers 
 0306  Hatch open 
 0312:50  EMU on bat 
 0313  Akers egress 
 0324  Thornton egress 
 0327  Thornton on MFR 
 0425?  HSP removed 
  HSP temp stow 
 0451  COSTAR removed from box 
 0539?  COSTAR installed 
 0619  HSP into box 
 0652  HSP stowage complete 
 0720  Thornton off MFR 
 0720  Akers on MFR 
 0730  Working on new coprocessor 
 0830  Coprocessor installed 
 0836  Akers off MFR 
 0838  KT on MFR 
 0940  PLB cleanup 
 0947  Thornton off MFR 
 0955  ingress 
 0957  Hatch closed 
 1003:42  Slow repress (6:58) 
 1006  0.5 psi 
 1010  2.3 psi 
 1012  5 psi (7:07) 
 1014  9.3 psi 
 1019  Inner hatch open 
 1606   96.46 585 x 593 x 28.5 
1993 Dec 9  0226  RCS reboost 61s 96.62 592 x 600 x 28.5 
 0317  Depress to 6psi 
 0320  Leak check problems 
 0324  Depress resume from 5psi 
 0326? Depressurized 
 0327:33  EMU on bat 
 0332  Hatch open EVA-5 
 0336  Hoffman egress 
 0347  Hoffman on MFR 
 0355  PDM auto deploy fails 
 0411  Hoffman off MFR 
 0415? Musgrave on MFR 
 0430  Working on SADE 
 0643  SADE electronics work complete 
 0700  RMS move MFR/Musgrave and Hoffmann to PDM 
  SADE changeout 
 0705  PDM manual deploy -V2 solar array 
 0725  PDM manual deploy +V2 solar array 
 0800 GHRS repair 
 0830  GHRS repair complete 
 0900 Magnetometer cover replacement 
 0930  Mag covers complete 
 1027 MFR ungrapple 
 1006  Begin SA II deploy, -V2? 
 1035  SA II deploy complete 
 1038  Ingress 
 1046.50  Hatch closed 
 1050:33  Repress (07:24) (offl. 07:21) 
 1052  Leak check 
 1057  Cabin pressure 
 1147  Solar arrays deployed and OK 
1993 Dec 10  0744:14 RMS grapple HST 
 0753:11  HST unberthed 
 0937  Aperture door opened 
 1026:47  HST released 
 1027:22  SEP1 burn 0.1m/s 
 1057:13  SEP2 burn 0.4m/s 
 1100? RMS berthed 
1993 Dec 13  0137  PLBD closed  96.60 591 x 599 x 28.5 
 0414:45  OMS deorbit 4:55 160m/s  52 x 596 x 28.5 
 0419:40  OMS DO CO 
 0454:41  Entry interface 
 0525:13  Gear down 
 0525:34  Landed RW33 KSC 
 0525:43  Drag chute out 
 0525:45  Nose gear touchdown 
 0526:11  Chute sep 
 0526:30  Wheels stop 
 0945Tow to OPF  OPF/1 

Friday, December 24, 1999

USA-118

 1996-026A


Titan 4 K-16/TC-15 was launched in Apr 1996 with a 23.2m fairing. It is believed to have carried a Mercury intelligence satellite to GEO.


USA 118 
 

DateTimeEventOrbit  

1996 Apr 24  2337:01  Launch by Titan K-16  CC LC41 
 2339  SRM sep 
 2341  Fairing sep 
 2342  Stage 1 sep 
 2346  Stage 2 sep, Centaur TIG1 
 2349  Centaur MECO-1  188 x 294? x 28.7  
1996 Apr 25  0138? Centaur TIG2  684.0 225 x 38455 x 28.6 (UN) 
 0139S? Centaur MECO2 
 0710? Centaur TIG3 
 0712? Centaur MECO3 
 0715? Centaur sep, payload in GEO 

Gambit-3 28

  1970-061A


KH-8 28 was launched on 1970 Aug 18 by Titan 3B Agena D from Vandenberg. In addition to its close-look imaging mission, it also carried an accelerometer to study the density of the Earth's atmosphere. Perigee of this mission, at 151 km, was higher than for any other KH-8 flight bar the first two test flights. Mission 4328 remained in orbit for 16 days of a planned 18-day mission, returning imagery of the Middle East including the Aug 1970 Suez ceasefire.


KH-8 28 
 

DateTimeEventOrbit  

1970 Aug 18  1445  Launch by Titan 3B Agena D  V SLC4W 
 1447  Titan stage 1 sep 
 1450  Titan stage 2 sep 
 1450  Agena burn 
 1455? Agena MECO 
 2312   89.48 130 x 366 x 111.0 
1970 Aug 19  0341   89.49 139 x 358 x 111.0 
  Raise apo 
1970 Aug 21  0459   89.64 149 x 363 x 110.9 
1970 Aug 23  1215   89.53 148 x 354 x 111.0 
  Raise apo 
1970 Aug 24  1513   89.94 149 x 393 x 110.9 
  Raise orbit 
1970 Aug 25  0016   90.46 151 x 442 x 111.0 
 1849?  SRV-1 recovery opp rev 116  
 1856?  Entry 
 1925?  SRV-1 recovered 
1970 Aug 25  2251   90.00 149 x 399 x 111.0 
1970 Aug 29  0017   89.60 147 x 361 x 111.0 
  Raise apogee
1970 Aug 30  2235   89.97 150 x 395 x 111.0 
1970 Sep 3  0430   89.77 150 x 376 x 111.0 
1970 Sep 4  1500 88.48 137 x 260 x 111.0 
1970 Sep 5
 1936? SRV-2 recovery opp rev 277 
 1943? Entry 
 2010? SRV-2 recovered 
 2108?  Deboost

Tuesday, December 21, 1999

Korolev : how one man masterminded the Soviet drive to beat America to the moon

 https://welib.org/md5/ab84efa51fcb7e23c495f811c431d994

Kosmos 598

  1973-072A


Kosmos-598 was launched in Oct 1973 and flew a 6 day mission.


Kosmos-598 
 

DateTimeEventOrbit  

1973 Oct 10  1045  Launch by 11A57  PL  
 1049  Blok-I burn  
 1053  Blok-I sep  
 1802   89.91 206 x 333 x 72.8 
 1900   89.94 208 x 334 x 72.84 (RAE) 
  Lower orbit 
1973 Oct 13  1141   88.99 207 x 241 x 72.8 
1973 Oct 14  0000   89.02 204 x 247 x 72.84 (RAE) 
 1721   88.98 202 x 245 x 72.9 
1973 Oct 15  0635?  Engine sep 88.92 199 x 242 x 72.85 (RAE) 
1973 Oct 16  0620? Retrofire 
 0630? PO sep 
 0634? Entry 
 0651? Landed after 5.8d 

Monday, December 20, 1999

Seventeen: April 1999

 https://welib.org/md5/291f5837cba8f317af7d677cbccd0e2a

STS-71 (Atlantis)

 1995-030A


The first docking between American and Russian spaceships in twenty years was the culmination of years of planning and the beginning of an expected long term integration of the American and Russian piloted space programs. Atlantis and Mir were easily visible to observers in the US and Western Europe in the hours before docking on 1995 Jun 29.

The payload bay of Atlantis contained a new element, the Orbiter Docking System (ODS). This was placed between the standard Tunnel Adapter and the Spacelab Long Tunnel, leading to a Spacelab long module placed unusually far back in the bay. An extra tunnel extension was used between the LT and the ODS. Atop the ODS a docking tunnel culminated in a Russian-build androgynous docking system designed for Buran and descended from the ASTP system.

The all-veteran crew of five NASA astronauts was commanded by former chief astronaut Hoot Gibson. Joining them aboard STS-71 as passengers were the Mir EO-19 crew, Anatoliy Solov'yov and Nikolai Budarin. The US crew included Bonnie Dunbar, who had trained as the backup for Mir EO-18 astronaut Norm Thagard. Thagard had been aboard Mir for over 100 days at the time of the Atlantis launch, together with Vladimir Dezhurov and Gennadiy Strekalov.

Launch of Atlantis was delayed several times but on Tuesday 1995 Jun 27 the weather cleared and OV-104 left the pad at the start of the seven minute long launch window. During the flight of the solid rocket motors, hot gas reached and charred the O-ring of an internal nozzle joint at the base of the left hand booster, the first O-ring damage since the loss of 51-L. This would lead to concerns for the STS-69 flight, but the Atlantis crew were oblivious to the the problem. Indeed, the damage was not discovered until the following mission, STS-70, had already reached orbit.

The R-bar rendezvous saw Atlantis within 100m of the station at around 1100 on Jun 29. At 1240 the Orbiter closed to 10m and paused for a few minutes before the final approach. Gibson flew the ODS into Kristall's clutches within five seconds of the target time; relative motion between the two hundred-ton space complexes was quickly damped out and by 1309 the hard dock was complete.

After pressure checks, the hatch was opened at 1500 UTC and Gibson and Dezhurov shook hands. All ten space travellers gathered in the Mir base module for mutual greetings and a photo opportunity, followed by a safety briefing. Finally, work began in the Spacelab module to prepare for the week's medical experiments.

Transfers to Mir included Russian and US EVA tools, Russian soft bag with pressure sealant, Russian food, TREK storage boxes, Mir-19 data file, and the PCG and SAMS experiments. Returned from Mir were a command processor, the Salyut-5B computer, surface and airborne samples, Spektr TORU boxes, urine bags, cold storage bio containers, water samples,and Spektr foam padding.

The next few days aboard the joint station, visible in the early evening skies over the United States as a brilliant star outshining Jupiter, included gift exchanges, press conferences, and farewell ceremonies as well as scientific experiments. Finally on Jul 3 the hatch to Atlantis was closed as the STS-71 crew and the returning EO-18 crew slept in the Shuttle, with the EO-19 crew sleeping aboard Mir.

Jul 4 saw some of the most spectacular images of the space program with three spacecraft involved in proximity operations. Solov'yov and Budarin undocked Soyuz TM-21 from the Kvant module, and backed off to 200m to observe the station. Budarin videotaped as Atlantis undocked from the Kristall module.

Atlantis slowly backed off to 200m and then began a 360 degree flyaround of the station. Meanwhile, Soyuz was reapproaching Kvant, when an attitude control computer on Mir crashed and the station began to drift away from its intended orientation. Solov'yov completed the redocking over a minute ahead of schedule, piloting the Soyuz to compensate for the rotating station and drawing on the experience of his six previous dockings with Mir.

Atlantis fired its engines at the completion of the flyaround, as the Mir crew reentered the station. The next several days saw extensive medical tests on the EO-18 crew, before the Spacelab module was deactivated for the last time. Reentry and landing were nominal, with Dezhurov, Strekalov and Thagard carried from the Shuttle on stretchers - although Thagard had reportedly been walking around on the Shuttle middeck shortly after landing. 


STS-71
 

DateTimeEventOrbit  

1995 Apr 20  1320  Roll to VAB  VAB 
1995 Apr 21   Mate to ET 
1995 Apr 26  0743  Rollout to LC39A 
1995 Jun 23   Scrub due to weather 
1995 Jun 24   Scrub due to weather 
1995 Jun 27  1932:19 Launch  

1934  SRB sep 123.56s 

1940  MECO 510.48s 
 1941  ET 70 sep  88.27 81 x 298 x 51.6 
 2015:16  OMS-2 48s 22m/s  89.02 158 x 294 x 51.6 
 2106  Payload bay open 
 2110? ET-70 reentry 
 2310:25  NC1 (OMS-3) 137s 67m/s 91.35 293 x 387 x 51.6 
1995 Jun 28  1049:35  OMS-4L 12s 3m/s  91.47 302 x 390 x 51.6 
1995 Jun 29  0758  NC4 (OMS-5 0:45) 23m/s 92.37 382 x 389 x 51.6 
 0931:02  TI, OMS-6L 9s 2m/s range 16km   
 1024  MC burn 
 1035  MC burn 

1050  R-bar rendezvous with Mir complex, 580m  92.48 393 x 399 x 51.6 
 1125  Begin stationkeeping at 82m 
 1223  Begin approach 
 1250  At 10 m from Kristall 
 1255  Resume approach 
 1300:05  Docked with Mir/Kristall  92.48 392 x 399 x 51.6 
 1308  Hard dock 
 1500  Hatch open to Kristall 
1995 Jul 3  1935  Hatch closed 
1995 Jul 4  1109:41  Undock 
 1138  At 200m distance, flyaround 
 1235  Complete flyaround, sep burn 
1995 Jul 5    92.44 390 x 398 x 51.7 
1995 Jul 7  1106  Payload bay doors closed 
 1345:19  OMS DO (3:32) 114m/s 48 x 398 x 51.7 
 1422  Entry interface 
 1454.36 Main gear touchdown, RW15 KSC 
 1454.39  Chute dep 
 1454.44  NGTD 
 1455.10  Chute sep 
 1455.27 Wheels stop 
 1830Tow OPF/2 

STS-55 (Columbia)

 1993-027A


The second German Spacelab mission, Spacelab D-2, flew on STS-55. DLR and ESA microgravity experiments were carried. The standard 5-tank PSRD set was carried, with no EDO pallet.

The first launch attempt, on 1993 Mar 22, ended in an RSLS abort at T-3 seconds, when SSME 2011 failed. The next attempt, on 1993 Apr 26, was successful. The Shuttle slowly gained altitude because of the MOMS pointings, and an RCS trim burn was carried out on Apr 29 to cancel the gain.


STS-55 mission events 
 

DateTimeEventOrbit  

1993 Feb 7   Rollout  LC39A 
1993 Mar 22  1450:53  SSME start 
 1450:57  RSLS abort, T-3  
1993 Apr 26  1449:54  SSME start 
1993 Apr 26  1450:00  Launch  LC39A 
 1452:05  SRB sep 
 1458:31  MECO  88.22 69 x 303 x 28.5  
 1458:49  ET sep 
 1529:55  OMS 2 2:20, 68m/s 90.55 299 x 303 x 28.47 
 1532:14  OMS 2 CO 
 1619  PLBD open 
 1859  Spacelab activate 
1993 Apr 27  0200?  RCS lower apogee90.53 297 x 303 x 28.47 
1993 Apr 29  0716   90.52 294 x 305 x 28.47 
1993 Apr 29  1224  RCS lower perigee 2 km  90.48 291 x 305 x 28.46  
1993 May 2  0559   90.46 288 x 305 x 28.46 
1993 May 5  2229   90.43 285 x 306 x 28.46 
1993 May 6  0625  Spacelab deactivate 
 0924  PLBD close 
 1329:20  OMS DO (2:53) 88m/s  18 x 291 x 28.5  
 1332:13  OMS DO CO 
 1358:35  Entry interface 122 km 
 1430:00  Landing  RW22 EAFB 
 1430:15  Drag chute out 
 1430:17  NGTD 
 1430:41  Drag chute sep 
 1431:02  Wheels stop 
1993 May 11  1730SCA takeoff  Edwards 
 2115SCA landing  Biggs AAF, El Paso 
1993 May 12  1430SCA takeoff  Biggs AAF 
 1545SCA landing  Kelly AFB TX 
1993 May 14  1310SCA takeoff  Kelly AFB TX 
 1500SCA landing  Columbus AFB MS 
 1620SCA takeoff  Columbus AFB MS 
 1825  SCA landing  KSC SLF 
 2300Tow to OPF  OPF/3 

Sunday, December 19, 1999

Mercury-Atlas 5

  1961-033A


The MA-5 flight carried the monkey Enos into orbit. The flight was cut short due to a thruster leak and the spacecraft splashed down after 3h 20m 59s. Enos returned to Holloman in Dec 1961.


MA-5 
 

DateTimeEventOrbit  

1961 Nov 29  1507:57  Launch by Atlas 93D 
 1510:08  T+2:11 BECO 62 km  
 1510:11  T+2:14 Booster sep 
 1510:31  T+2:34 Tower jettison 90 km  
 1512:57 T+5:00 MECO 161 km  
 1513:00 T+5:03 Atlas D sep  158 x 237 x 32.6 
 1808:12  T+3:00:15 Retrofire 
 1809:12 T+3:01:15 Retropack sep  -195? x 174 x 32.6 
 1817:38  Reentry T+3:09:41  
 1828:56  T+3:20:59 Splashdown at 28 57 N 66 04W 
 1944  Recovered by USS Stormes 

July 11,1998

 https://planet4589.org/space/jsr/back/news.366.txt

Anik A2

  1973-023A


Anik A-2 (Telesat B) was placed at 109W until 1979, when it moved to 106W. In 1981 it was colocated with Anik A-3 at 114W, and was retired in 1982. As well being part of the Canadian telecom system, Anik A-2 was used for RCA's Satcom Phase I, inaugurating the RCA Satcom system prior to the launch of Satcom I.


Anik A-2 
 

DateTimeEventOrbit  

1973 Apr 20  2347:03 Launch by Delta 1914  CK LC17B 
  T+0:38 SRM 1-6 off 
  T+0:39 SRM 7-9 on 
  T+1:17 SRM 7-9 off 
  T+1:25 SRM sep 
  T+4:18 MECO 
  T+4:24 VECO 
  T+4:26 St 1 sep 
 2351:34 T+4:31 Stage 2 SES-1  
  T+4:55 Fairing 
 2356:57 T+9:54 Stage 2 SECO168 x 222 x  
 0010:25 T+23:22 St 2 sep 
1973 Apr 21  0010:38 T+23:35 Star 37E burn 44s 
 0011:22 T+24:19 Star 37E burnout 
 0011:42 T+24:39 SES-2 engineering, dV=462.7m/s 
 0011:56 T+24:53 SECO-2  216 x 2784 x 29.49  
 0013:03 T+26:00 Star 37E sep  212 x 36480 x 26.7 
1973 Apr 23  2200  FW5 burn 42s apo 7 at 158W 1430.7 35604 x 35709 x 0.1 
1973 May 6   On station  GEO 109W 
1975 Dec 30    GEO 109W (Morgan) 
1977 Jan 25  0133   1436.08 35780 x 35792 x 0.0 GEO 109.0W 
1977 Dec 31    GEO 109W (Morgan) 
1979 Apr 5    1436.09 35784 x 35788 x 0.0 GEO 108.5W 
1979 May   Move to 106W 
1979 May 30    1436.11 35771 x 35802 x 0.0 GEO 106.4W 
1980 May 3    1436.09 35778 x 35794 x 0.1 GEO 106.4W 
1981 Jan 14    1436.10 35778 x 35794 x 0.1 GEO 106.6W 
1981 Jan 15   mv out  
1981 Jan 18    1437.20 35778 x 35838 x 0.1 GEO 106.6W+0.3E 
1981 Feb 10    1437.27 35780 x 35838 x 0.0 GEO 113.4W+0.3E 
1981 Feb 17   Colocate Anik A-3  GEO 114W 
1981 Mar 9    1436.07 35779 x 35792 x 0.0 GEO 114.0W 
1981 Jun 1    GEO 114W 
1982 Oct 1    GEO 114W 
1982 Oct 14    1436.11 35780 x 35793 x 0.2 GEO 114.0W  

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...