Tuesday, December 22, 1998

Kosmos 2307

 1995-009A


Three Uragan class navigation satellites built by AKO Polyot were launched on 1995 Mar 7 to become part of the Glonass system. According to the Russian Space Forces, the satellites are Glonass numbers 765, 766 and 777. The satellites are in 12-hour, 19000 km high orbits. Launch was by a Proton-K with a Blok-DM2 upper stage.


Kosmos-2307 
 

DateTimeEventOrbit  

1995 Mar 7  0923:44  Launch 
  T+2:07 St 1 sep 
 0927 T+3:20 GO sep 
  T+5:38 St 2 sep 
 0933  T+9:40 St 3 MECO? 
 0933  T+9:52 St 3 sep 
 0933  T+10? Perekhodnik sep from DM2 
 1025  T+1:01:58 DM burn 1 
 1031 T+1:07:50 DM MECO1 
 1318 T+3:54:48 DM burn 2 
 1320 T+3:57:14 DM MECO2 
 1320  T+3:57s KA-1 sep 
1995 Mar 30   In service 

Monday, December 21, 1998

Kosmos 1166

 1980-020A



Kosmos-1166 
 

DateTimeEventOrbit  

1980 Mar 4  1030 Launch by Soyuz-U  Plesetsk 
 1038  Blok-I burn 
1980 Mar 5  90.28 196 x 379 x 72.9 
1980 Mar 6   Orbit raise  92.25 354 x 415 x 72.9 
1980 Mar 15  92.25 355 x 414 x 72.9 
1980 Mar 18   
 0425?  Deorbit 
 0436? PO sep 
 0452? Entry 
 0508?  Landed 

Reference Books Bulletin, 1997-98: A Compilation of Evaluations September 1997 Through August 1998

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Gals 1

 1994-002A


Gals 1 (Gals No. 11) was developed by NPO-PM for improved television broadcasting. It was intended to be stationed at 44E. By the time it was ready, Russia's economic troubles prevented its use domestically and it was bought by the Land Group (Land Commercial Satellite Corporation), a Beijing-based consortium. The satellite was contracted and delivered on orbit by AO Informkosmos, which was a consortium of NPO PM, NII Radio, NII for Space Instruments, and the Moscow NI Radiotechnical Institute.  It is controlled from the NPO PM TsUP. The satellite had a mass of 2500 kg and the launch was the first use of the Blok DM-2M upper stage. Gals No. 11 uses the MSS-2500-01-GEO bus. The satellite was flight tested at 71E and then moved to 36E. Space Command orbital data show the satellite at the old position up to May 1996, but this is likely to be incorrect. The Land group's Roosevelt Commercial Satellite Co. leased capacity to Loral and GT/Asian TV. In 1996, Land Group chairman Mou Qizhong reportedly relocated the Land satellite management to Hong Kong, but I have not confirmed this. In 1999 Gals 1, which was then carrying the Russian NTV+ channel, was reportedly retired, although the orbital position was maintained during 1999 and NK reported it still in Intersputnik service in 2000.


Gals 1 
 

DateTimeEventOrbit  

1994 Jan 20  0949 Launch by Proton-K  KB 
  Stage 2 burn 
  Stage 3 burn 
 0958  Stage 3 sep 
 0958 Adapter sep  185? x 190? x 51.6 
 1102? DM-2M burn 1 
  DM-2M MECO-1  190? x 36000? x 47.4 
 1620? DM-2M burn 2 
 1630? DM-2M sep 
1994 Jan 20    1446.74 35908 x 36081 x 0.3 GEO 91.1E+2.7W 
1994 Jan 22    1451.15 36063 x 36098 x 0.3 GEO 83.3E+3.7E/d 
1994 Feb 1    1443.03 35890 x 35954 x 0.2 GEO 49.7E+1.7E/d 
1994 Feb 13    1435.91 35779 x 35786 x 0.2 GEO 44.3E + 0.01/d 
1994 Mar 21    1436.04 35779 x 35791 x 0.1 GEO 44.0E + 0.00/d 
1994 May 27   mv out 1434.33 35643 x 35860 x 0.1 GEO 45.4E +0.4W/d 
1994 Jun 12    1432.40 35679 x 35749 x 0.1 GEO 70.6E+0.9W/d 
1994 Jun 14    1435.94 35774 x 35793 x 0.1 GEO 70.8E 
1994 Jul 4   mv in  1436.05 35774 x 35797 x 0.1 GEO 71.4E 
1994 Jul 29    1436.28 35776 x 35803 x 0.2 GEO 70.6E 
1994 Aug 27    1436.09 35780 x 35792 x 0.1 GEO 71.3E 
1995 Jul 18    1436.08 35774 x 35798 x 0.0 GEO 70.9E 
1996 May   Move to 36E? 
1996 May 30   
1436.07 35784 x 35787 x 0.1 GEO 71.0E 
1996 Jun 1    1436.10 35781 x 35787 x 0.1 GEO 35.8E 
1996 Jul 20    1436.05 35775 x 35796 x 0.1 GEO 36.0E 
1998 May 1    1436.15 35780 x 35795 x 0.4 GEO 36.1E 

Palm Beach facts & fancies, caprices & curiosities

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Molniya 167

 1986-057A


Molniya-1 (F73, N67) was launched on 1986 Jul 30 from Plesetsk. It replaced N59 in the E plane.


Molniya-1 F73 
 

DateTimeEventOrbit  

1986 Jul 30  1506:00  Launch by Molniya 8K78M  PL 
  BVGD sep 
  GO sep 
  T+4:46 Blok A sep 
  T+4:56 KhO sep 
  T+8:46 Blok-I MECO 
 1514  T+8:50 Blok-I sep 
  T+53:16 BOZ burn 
 1600? T+53:56 BOZ sep 
  ML burn 
  T+56:46 ML MECO 
 1603?  T+56:54 ML sep   
   200 x 641 x 62.8 (B) 
1986 Jul 30  1700   618 x 40626 x 62.7 
1986 Aug 4  1700   622 x 39782 x 6

Kosmos 1517

 1983-125A


The third orbital test switched to a Black Sea recovery after one rev, possibly due to the Australian Navy's photography of the Indian Ocean recovery. The time from 100 km entry to 40 km test point was much longer, around 24 minutes, as the vehicle covered an 8000 km range across Europe.


BOR-4 Flight 3 
 

DateTimeEventOrbit  

1983 Dec 27  1000 Launch by K65MP GTsP4 
 1002? Stage 2 burn 
 1008? Stage 2 sep 
 1100?  88.5 180 x 221 x 50.7 
 1106? Deorbit 
 1122? 100 km  
 1124?  Entry 
 1150? Landed in Black Sea 

STS-51 (Discovery)

 1993-058A


STS-51 suffered an RSLS abort on Aug 12, but successfully took off a month later on a mission to deploy the ACTS communications satellite and fly the ORFEUS-SPAS experiment. After a one-orbit delay due to comm problems ACTS/TOS was ejected from its cradle. Because of a command error, the explosive separation tube was more powerful than intended and left sharp edges and debris on the support cradle and in the payload bay to the rear of bay 10.


STS-51 
 

DateTimeEventOrbit  

1993 Jun 19   Tow to VAB/1 
1993 Jun 20   ET mate 
1993 Jun 28   Rollout  LC39B 
1993 Aug 12  1312:28  SSME ignition 
 1312:32  SSME shutdown, RSLS 
1993 Sep 12  1145:00  Launch from LC39 
 1147:05  SRB sep 
 1153:31  MECO 
 1153:49  ET sep  88.18 67 x 302 x 28.5 
 1208:31  ET doors closed 
 1224:54  OMS-2 2:25 68m/s 
 1227:20  OMS-2 CO 
 1327  PLBD open  90.52 296 x 302 x 28.47 
 1700?  RMS checkout 
 1856  ASE unlatch 
 1902  Clamshell open 
 1908  Tilt table raised 
 2113:28  ACTS/TOS deploy 
 2113:55  RCS sep 1m/s 
 2130:28  OMS-3R sep (0:28) 7m/s  90.77 297 x 327 x 28.46  
 2130:57  OMS-3 CO 
 2152  RMS unstow to observe TOS burn 
 2158:35  TOS burn (1:40) 
 2230?  RMS restow 
1993 Sep 13   RMS unstow 
 0923:29 OMS-4L 46s 12m/s 
 0923:47  OMS-4 CO 
 0954:18  RMS grapple SPAS 
 1000   90.33 273 x 308 x 28.5 
 1244:07  RMS unberth SPAS 
 1342  SPAS door tests 
 1505:59  Deploy SPAS  90.32 271 x 307 x 28.46 
1993 Sep 15  0600   90.30 274 x 304 x 28.5 
1993 Sep 16  0818:20  Begin AL depress 
 0829:45  Airlock depress (STSMR) 

 

0829  HO  
1993 Sep 16  0832  EVA Walz, Newman 
 0839  Egress 
 0905  PLB setup 
 0927  Walz gathering ratchet tools in airlock 
  Translation adaptation 
  High torque ratchet test at mini-ws. 
 1026  Newman working on HST PFR install 
  HST tool testing
 1230  Walz starting HST PFR eval 
 1320  Cleanup work area 
 1350  PLB cleaned up, PSA stowed 
 1407  EV crew sightseeing 
 1515  Ingress 
 1523  Prep for HC 
 1525  HC, prep for repress 
 1537  Repress (7:05:28) (STSMR) 90.30 271 x 307 x 28.46 
  RCS skeep SPAS 
1993 Sep 17  0632:44  OMS-5L 7s 2m/s 
 0632:51  OMS-5 CO 
 0710   90.35 277 x 306 x 28.46 
 1106:56  OMS-6R SPAS approach 7s 2m/s 
 1107:03  OMS-6 CO 
 1328   90.28 270 x 305 x 28.46 
1993 Sep 18  1454   90.26 268 x 306 x 28.46 
1993 Sep 19  0530?  RCS approach 
 0938:35  TI burn  
 1000  MC1 (1s) 
 1029  MC2 (6s), 10 km 
 1040  MC3 (2s)  
 1043  Tally Ho 
 1050  MC4 (1s), on manual  90.26 269 x 305 x 28.46 
 1118  V-bar, 100m 
 1149:33  RMS grapple SPAS 
 1330  RMS WSF free drift test 
 1405:44  RMS berth SPAS 
 1420  RMS ungrapple SPAS 
 1430?  RMS reberthed 
 1544   90.25 267 x 305 x 28.5  
1993 Sep 20  0445  RMS used for PLB survey 
 0525  RMS reberthed 
1993 Sep 21  0558  PLBD closed 
 0946  PLBD open, waveoff 
1993 Sep 22  0423  PLBD closed  90.25 266 x 306 x 28.5 
 0655:30  OMS DO (2:17) 77m/s  19 x 270 x 28.5 
 0657:48  OMS DO CO 
 0724:40  Entry 
 0730  80 km 
 0756:06  Landed RW15 KSC 
 0756:17  Chute 
 0756:22  NGTD 
 0756:45  Chute out 
 0756:55  Wheels stop 
 1030Tow to OPF/3 

Tiros 2

  1960-016A


Before launch, this payload had two names: A-02 in the old NASA system, and Tiros B in the new one. The second of the original hatbox-class Tiros, it carried IR radiometers in addition to the 2 TV cameras. Tiros 2 demonstrated magnetic attitude control and an extended satellite lifetime, operating for one year in space. The satellite measured ice pack conditions in the St. Lawrence and its data was used to forecast the end of a heat wave in Australia. Tiros 2 was also used for weather forecasting support for MR-3 and Ranger 1. Mass was 122 kg, size 0.48m high, 1.1m dia.

Tiros II was launched on 1960 Nov 23 at 1112; at 1115 the Thor first stage cut off after a 158s burn, and the Delta second stage began its 109s burn. The Tiros/Altair/Delta combination coasted for 7.5 min from 1117 to 1124 when the Delta separated and the Altair burned for 42s. After a further 2 min coast period the Altair separated and Tiros II was in its 619 x 732 km x 48.5 deg orbit. It operated until 1961 Dec 4, transmitting limited data until May 1962. By Dec 1993 the orbit had decayed to 547 x 610 km x 48.5 deg.


Tiros 2 
 

DateTimeEventOrbit  

1960 Nov 23  1113:03  Launch by Delta  CC LC17A 
 1115  T+2:38 Thor MECO 
 1115  Delta S/N 2013 SES 1:49 
 1117  Delta SECO 
 1124  Delta sep 
 1124  Altair S/N 106 burn 42s 
 1124  Altair burnout 
 1126  Altair sep, spin at 126 RPM 
  Despin weights release 
1960 Nov 25   Spin rockets fire 
1961 Dec 4   End of tx 

Payload:

  • TV Cameras (2)

  • Scanning IR Experiment (NASA/)

  • 5 Channel Radiometer

  • 2 Channel Radiometer

Progress M-10

 1991-073A


Progress M 11F615A55 No. 211 (Progress M-10) was launched on 1991 Oct 17. It carried a VBK. At undocking, Progress M-10 carried out the Mgnovenie experiment. The crew photographed the Progress as it passed over the horizon, using a Hasselblad camera with special light filters, to study absorption by the ozone layer. The VBK landed at 51 41 N 73 21 E, 229 km N of Karaganda.


Progress M-10 
 

DateTimeEventOrbit  

1991 Oct 17  0005:25  Launch by Soyuz-U  KB 
 0230   88.60 183 x 226 x 51.65 
1991 Oct 19  0215  Rendezvous with Mir, docking aborted at 150m 
1991 Oct 21  0340:50  Docked with Mir DP1  
 1200   92.53 395 x 401 x 51.61 
1991 Nov 1    92.46 391 x 398 x 51.60 
1992 Jan 20    92.09 376 x 378 x 51.60 
 0715:44  Undocked 
  Mgnovenie experiment 
 1120?  deorbited  
 1144?  VBK ejected 
 1203:30  VBK landed in Kazakhstan 

Sunday, December 20, 1998

Vortex 10

 1981-107A


The third VORTEX mission was launched by Titan 3C in October 1981. This was the first flight of the AJ10-138A ITIP transtage engine.


VORTEX 10 
 

DateTimeEventOrbit  

1981 Oct 31  0922:01  Launch by Titan IIIC  CC 
  T+1:50 Stage 1 ignition 
  T+2:02 SRM sep 
  T+4:35 St 1 sep 
 0926 T+4:45 Fairing sep 
 0930  Stage 2 MECO 
 0930  T+8:05 Stage 2 sep  134 x 382 x 29.3 (UN) 
   89.36 147 x 338 x 29.3 (TLE/Nov 1) 
 0944?  Transtage burn 1 
 0947? MECO-1  190? x 40100? x 27? 
 1542?  Transtage burn 2 
 1545?  Transtage sep 
1981 Nov 1  GEO 
1983 Apr  32000? x 40100? x 7.5? (guess) 
2006 Jul 17    1436.92 31728 x 39876 x 7.3

Soyuz T-9 (Proton)

 1983-062A



    Crew

  • Komandir Pol. Vladimir Lyakhov, VVS

  • Bortinzhener Aleksandr P. Aleksandrov, NPO Energiya


Soyuz T-9, Flight 1 
 

DateTimeEventOrbit  

1983 Jun 27  0912:18 Launch by Soyuz-U  KB 
 0914 Blok-BVGD sep 
 0917  Blok-A sep  
 0920  Blok-I cutoff 
 0920  Blok I sep 
  Blok-I sep  88.7 199 x 228 x 51.6 
   90.0 254 x 303 x 51.6 
   90.1 260 x 304 x 51.6 
1983 Jun 28   90.6 281 x 322 x 51.6 
 1046  Docked with Salyut-7 +X 
   324 x 336 x 51.6 


Soyuz T-9, Flight 2 
 

DateTimeEventOrbit  

1983 Aug 16  1425  Undocked from Salyut-7 +X 
 1445?  Docked at Salyut-7 -X 


Soyuz T-9, Flight 3 
 

DateTimeEventOrbit  

1983 Nov 23  1640  Undocked from Salyut-7, -X 
 1743? BO sep 
 1912?  Deorbit 
 1916?  DO CO 
 1929?  PAO sep 
 1935?  Entry 
 1958  Landed 

Telstar 303

 1985-048D


The final AT&T; HS-376 based Telstar, 3D or 303, was deployed on Shuttle mission 51-G.


Telstar 303 
 

DateTimeEventOrbit  

1985 Jun 19  1120  Deploy from OV-103 

1205  PAM-D burn 
 1206  PAM-D burnout 
 1208  PAM-D sep
1985 Jun 19    664.79 394 x 37313 x 25.5 
1985 Jun 19    662.88 360 x 37250 x 25.4 
1985 Jun 20  1505  Star 30BP burn 
1985 Jun 21    1410.25 33327 x 37230 x 0.2 GEO 64.9W+6.6E 
1985 Jun 24    1435.93 35122 x 36444 x 0.3 GEO 61.7W+0.04E 
1984 Jun 30    1436.07 35128 x 36444 x 0.3 GEO 60.9W 
1985 Jun   Tests  GEO 62W 
1985 Jul 16   mv out  1451.30 35711 x 36455 x 0.2 GEO 62.3W+3.8W 
1985 Aug 2   mv in, on station  GEO 125W 
1985 Aug 5    1436.18 35783 x 35793 x 0.1 GEO 125.1W 
1985 Sep    GEO 126W 
1986 Oct 28    1436.07 35782 x 35789 x 0.1 GEO 125.0W 
1989 May 2    1436.09 35781 x 35791 x 0.0 GEO 125.1W 
1990 Aug 11    1436.06 35766 x 35804 x 0.0 GEO 125.0W 
1992 Apr 29   mv out 1436.02 35779 x 35780 x 0.0 GEO 124.9W 
1992 May 26   mv in 1436.06 35774 x 35797 x 0.1 GEO 123.1W 
1993 Jun 14    1436.08 35779 x 35792 x 0.0 GEO 123.0W 
1995 Feb 4    1436.07 35782 x 35789 x 0.0 GEO 123.1W 
1996 May 8   mv drift 1436.03 35779 x 35790 x 0.8 GEO 122.8W 
1996 Jul 24   mv in  1436.06 35776 x 35795 x 0.9 GEO 120.0W 
1997 Apr 15    1436.08 35779 x 35793 x 1.5 GEO 120.0W 

Aviation Week: August 17,1998

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Soyuz T-6 (Pamir)

 1982-063A


7K-ST (11F732) No. 9L was assigned to the joint Soviet-French mission, crewed by Vladimir Dzhanibekov, Aleksandr Ivanchenkov and Jean-Loup Chretien. It was launched on 1982 Jun 24 and named Soyuz T-6.


Soyuz T-6, Flight 1 
 

DateTimeEventOrbit  

1982 Jun 24  1629:51  Launch by Soyuz-U KB 
 1631:00  Blok-B,V,G,D sep T+1:09 
 1634:28  Blok-A sep T+4:35 
 1638:28  Blok-I sep, T+8:37 EOI 
   220 x 248 x 51.6 
   248 x 277 x 51.6 
   295 x 314 x 51.6 
1982 Jun 25  1709  Range 11 km, rdot 18 m/s 
 1719  Braking burn  
 1726  Range 1.4 km 
  Range 960m, braking burn  
 
Computer and Igla shutdown, manual control 
 1728  LOS 
 1736  AOS, range 100m stationkeeping 
 1743Final approach 
 1746  Docked with Salyut-7 +X 


Soyuz T-6, Flight 2 
 

DateTimeEventOrbit  

1982 Jul 2  1103:48  Undocked +X 
 1205  BO sep 
 1224:40  Descent program on  283 x 319 x 51.6  
 1334:40  Retrofire, 200s burn 
 1338:00  DO CO  -76 x 294 x 51.6 
 1346:47  PAO sep 
 1357:13  Entry 
 1421:10  Landed at 50 39 N 67 30 E

Tuesday, December 15, 1998

Electronic Publishing on CD-ROM

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Essex County Country Club : New Jersey's first country club

 https://welib.org/md5/ce338b422391aeb59296153151bbbfe8

People: June 22,1998

 https://welib.org/md5/48d7714ebcae6fa5dc1b9104d629c9b7

Skynet 2A

  1974-002A


The Skynet 2 series was built by Marconi for the Ministry of Defence Procurement Executive (MOD/PE). Skynet 2 was built in Portsmouth, with the hydrazine RCS built at Mytchett. Skynet 2A, planned for geostationary orbit at 40 deg E, was launched in Jan 1974 by a Delta 2313. (TR-1022 gives AJ10-118F as second stage, but this is probably an error). The Delta's second stage malfunctioned, burning for only 17s instead of 30s on its second burn, leaving the satellite and third stage in a low orbit. The satellite was not acquired by NORAD until Jan 23, and on Jan 24 an attempt was made to raise the orbit with the spacecraft kick motor. This maneuver was modified in real time by ground controllers to ensure a safe reentry of the space vehicle after it became clear that the orbit was untenable.


Skynet 2A 
 

DateTimeEventOrbit  

1974 Jan 19  0138:47  Launch by Delta 2313  CC LC17 
  T+0:38 SRM 1-3 out 
 0140  T+1:10 SRM 1-3 sep 
 0142:38 T+3:48 MECO 
  T+3:51 VECO 
 0142:42 T+3:56 St 1 sep 
 0142:48  T+4:01 Delta stage 2 SES-1 burn 5:25? 
 0148:02  T+9:15 Delta SECO-1  184 x 184? x 28.7 
 0200  AOS
 0200:34 T+21:47 SES-2, tumbling 
 0200:51 SECO-2 after 17s 
 0201:44? T+22:57? Delta sep  184 x 184 x 28.69 
 0202:21 T+23:34 Star 37D burn   
 0203:06 T+24:19 Star 37D shutdown  113.50 123 x 2261 x 37.7 
 0204:22 T+25:35 Star 37D sep 
1974 Jan 20  1700   121.48 96 x 3406 x 37.6 (rough) 
1974 Jan 24  0820Telemetry activated  104.12 101 x 1805 x 37.5 
 1237?  Star 24 burn, tumbled   

1974 Jan 25  

0350?Reentered over Pacific

November 20,2006

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