Sunday, July 28, 1991

Kosmos 609

  1973-092A


Kosmos-609 was launched in Nov 1973 and was a Zenit-4M flight from Baikonur at 70 deg. The Kettering group recorded a TK type recovery beacon.


Kosmos-609 
 

DateTimeEventOrbit  

1973 Nov 21  1000:00  Launch by 11A57  KB
 1004  Blok-I burn 
 1008  Blok-I sep 
1973 Nov 22  0930  90.1 241 x 314 x 70.0 (RAE)  
  Lower orbit 
1973 Nov 22  1900  89.7 174 x 341 x 70.0 (RAE) 
1973 Nov 23  1547   89.62 173 x 338 x 69.9 
1973 Nov 27  1352   89.53 172 x 329 x 69.9 
  Lower apogee 
1973 Nov 29  1505   89.13 172 x 290 x 69.9 
1973 Dec 2 
 89.06 174 x 281 x 69.9 
1973 Dec 3  0639? Engine sep  
1973 Dec 4  0623? Retrofire 
 0633? PO sep 
 0638? Entry 
 0654? Landed after 12.9d 

Friday, July 26, 1991

Kosmos 188

  1967-107A


Spacecraft 5 had originally been prepared for launch as Soyuz-2 during the Soyuz-1 mission. It was recycled for the automatic docking mission and launched as Kosmos-188. 7K-OK No. 5 (Kosmos-188) completed the first Soviet docking with 7K-OK No. 6 (Kosmos-186), only an hour after its launch on 1967 Oct 30. The docking was only a soft docking; a problem later to surface on Soyuz-10 prevented a complete seal.

The ion orientation system was used for deorbit, but locally low ion flux threw ite sensor off and the entry path was shallow and heading for impact east of Ulan-Ude. The APO self destruct system fired 60 km over Irkutsk.


Kosmos-188 
 

DateTimeEventOrbit  

1967 Oct 30  0812:41  Launch by 11A511 Soyuz  KB LC1 
 0817  Blok-I burn 
 0821  Blok-I sep; 24 km from K186 
 0920  Docked with 7K-OK No. 6  88.79 180 x 249 x 51.65 
 1250  Undocked  88.87 183 x 255 x 51.72 
 2248   88.97 192 x 255 x 51.72 
1967 Nov 1  0126?  88.84 190 x 245 x 51.64 
1967 Nov 2  0703  Deorbit 
 0715?  BO, PAO sep 
 0725?  Reentry over Irkutsk 

Raduga 12

 1983-028A


Raduga (Gran') No. 23 was launched in Apr 1983 to the Statsionar 3 position at 84E, replacing Raduga No. 17.


Raduga No. 23 
 

DateTimeEventOrbit  

1983 Apr 8  0445 Launch by Proton-K  KB 
 0454  Stage 3 sep 
 0602? DM burn 1 
 1118? DM burn 2 
 1122? DM sep 
1983 Apr 8    1441.15 35823 x 35947 x 0.7 GEO 90.7E-1.3W 
1983 Apr 22   On station at Statsionar 3  1436.0 min GEO 84E 
1983 Apr 23    1435.98 35779 x 35780 x 1.2 GEO 84.4E 
1983 Oct 11    1436.19 35756 x 35820 x 0.8 GEO 84.7E 
1984 Apr 22   last mv  1436.05 35757 x 35814 x 0.4 GEO 85.2E 
1984 May 30    1436.18 35773 x 35802 x 0.3 GEO 84.9E 
1984 Aug 21    1436.36 35774 x 35808 x 0.1 GEO 81.2E dr 
1984 Sep    GEO 86E 
1984 Oct   
GEO dr 
1984 Nov 20    1436.43 35763 x 35822 x 0.2 GEO 74.0E+0.1W 
1985 Dec 8    1435.76 35767 x 35792 x 1.2 GEO 76.7E 
1986 Oct    GEO 79E+0.1/d 
1987 Feb    GEO 68E+0.1/d 
1988 May 14    1436.03 35775 x 35794 x 3.5 GEO 84.6E 

Kosmos 1201

 1980-061A



Kosmos-1201 
 

DateTimeEventOrbit  

1980 Jul 15 0730 Launch by Soyuz  Plesetsk 
 0734? Blok-I burn 
 0738? Blok-I sep 
1980 Jul 15    88.97 209 x 236 x 82.3 
1980 Jul 16    88.94 211 x 232 x 82.3 
1980 Jul 22    88.80 203 x 226 x 82.3 
1980 Jul 24    88.74 201 x 222 x 82.3 
1980 Jul 27   
88.89 198 x 239 x 82.3 
1980 Jul 28  
 0332?  Deorbit 
 0343? PO sep 
 0348? Entry 
 0405? Landed 

Tuesday, July 23, 1991

Kosmos 360

  1970-068A


Kosmos-360 was launched in Aug 1970 from Baikonur. The fifth Zenit-4M mission lasted 10 days and seems to have been mostly successful.


Kosmos-360 
 

DateTimeEventOrbit  

1970 Aug 29  0830:00  Launch by 11A57  KB 
 0834  Blok-I burn 
 0838  Blok-I sep 
 2147   89.43 206 x 285 x 65.0 
1970 Aug 31?   Raise apogee 
1970 Aug 31  1701   89.65 203 x 310 x 65.0 
1970 Sep 4  0441   89.60 206 x 303 x 65.00 
  Lower apogee 
1970 Sep 5  0258   89.01 199 x 251 x 65.00 
1970 Sep 6  1136   88.97 200 x 247 x 65.0 
1970 Sep 7  0930  Engine sep (68C)
1970 Sep 8  0524?  Retrofire 
 0534? PO sep 
 0540? Entry 
 0556? Landed 

Monday, July 22, 1991

Interkosmos 24

 1989-080A


Interkosmos-24 and its subsatellite Magion-2 were launched as the Aktivniy-IK project to carry out active experiments in the magnetosphere. A plasma wave generator and a neutral gas injector were used to create magnetospheric disturbances whose effects were then measured.

Mass 1400 kg. Size 23m long with antennae, 4.0m span with antennae. The bus was 1.0 x 2.6m in size.


Interkosmos-24 
 

DateTimeEventOrbit  

1989 Sep 28  0004:59 Launch by Tsiklon-3  NIIP-53 
  T+2:00 St 1 sep 
  T+3:36 GO sep 
  T+4:42? St 2 sep 
  T+5:02? S5M burn 1 75s 
 0011? T+6:17? S5M MECO-1 
  T+25:00? S5M burn 2 35s 
  T+25:35? S5M MECO-2 
 0031?  T+26:05? S5M sep 
1989 Oct 3   Magion-2 deployed 
1989 Oct 4    115.91 500 x 2492 x 82.6 

Kosmos 103

  1965-112A


The first Strela-2 satellite was Kosmos-103, launched in Dec 1965 by 65S3 from Baikonur into a 600 km, 56 degree orbit.


Kosmos-103 
 

DateTimeEventOrbit  

1965 Dec 28  1230  Launch by 65S3  KB 
 1232  Stage 2 burn 
 1237  Stage 2 MECO 
 1300?  Stage 2 burn 2 
  Stage 2 sep  96.95 594 x 636 x 56.1 
   
1990 Jan 2   Reentered  87.57 151 x 156 x 56.0 

Thursday, July 18, 1991

Kosmos 1368

 1982-046A


Two-tone telemetry; Hi res satellite


Kosmos-1368 
 

DateTimeEventOrbit  

1982 May 21 1240 Launch by Soyuz-U  Baikonur 
 1244 Blok-I burn 
 1248  Blok-I sep 
1982 May 21    90.02 209x343x70.4 
1982 May 22    90.29 238x339x70.4 from 90.04 212x341 
1982 May 23  89.94 238x306x70.4 
1982 May 25    89.46 235x261x70.4 from 89.91 238x303 
1982 May 28    90.50 236x262x70.4 from 89.45 234x260 
1982 May 30    89.30 232x248x70.4 from 90.49 236x362 
1982 Jun 2  89.25 230x245x70.4 
1982 Jun 3  
 1000? Deorbit 
 1012? PO sep 
 1017? Entry 
 1035? Landed 


Aviation Week: September 3,1990

 https://welib.org/md5/621ce4626f67c59a23189013b62da6f9

Monday, July 15, 1991

Raduga 7

 1980-081A


Raduga (Gran') No. 17 was launched in Oct 1980 to the Stastionar 3 position at 85E.


Raduga No. 17 
 

DateTimeEventOrbit  

1980 Oct 5  1710 Launch by Proton-K  KB 
 1719 Stage 3 sep 
 1827? DM burn 1  627.29 209 x 35581 x 48.8 
 2343? DM burn 2 
 2347? DM sep 
1980 Oct 22    1436.00 35736 x 35832 x 0.6 GEO 84.4E 
1980 Nov 19    1436.06 35753 x 351818 x 0.3 GEO 85.3E 
1981 Apr 13    1436.23 35737 x 35841 x 0.0 GEO 84.4E 
1981 Jun 27    1436.10 35728 x 35844 x 0.1 GEO 86.2E 
1981 Aug    GEO 87E 
1981 Aug   mv out, drift W 
1981 Sep 12   drift 1436.90 35353 x 36251 x 0.1 GEO 78.5E+0.2W 
1982 Apr 12    1437.15 35743 x 35870 x 0.0 GEO 16.5E+0.3W 
1982 Sep 18   Mv in to Statsionar 8 pos.  GEO 26W 
1982 Nov 16    1436.09 35782 x 35790 x 1.3 GEO 24.7W 
1983 Jan    GEO 25W 
1984 Jan 4    1436.15 35776 x 35799 x 2.3 GEO 24.1W 
1985 Jan 26    1436.23 35779 x 3579 x 3.3 GEO 25.2W 
1985 Jul 10    1435.94 35772 x 35794 x 3.6 GEO 25.5W+0.03E 
1986 Jun 18    1436.31 35772 x 35809 x 4.5 GEO 26.2W+0.06W

Monday, July 8, 1991

Gemini 8

  1966-020A


The Gemini Titan Agena 8 mission was an important milestone in space technology and the race to the Moon. For the first time, two spacecraft were linked together in orbit. The Agena target was orbited first, followed by Gemini spacecraft 8. 

After rendezvous, Gemini 8 spent time stationkeeping while waiting for the RKV tracking ship to come into range,after which they approached the Agena.

At 2340 a stuck thruster on Gemini put the docked craft into a tumble. Armstrong, suspecting the Agena to be at fault, undocked, and the Gemini began to spin more rapidly. Armstrong had to use the reentry thrusters to cancel the spin, which by the mission rules mandated an emergency end to the mission.

The retrofire came over south China and Gemini VIII splashed down in the East Pacific. The spacecraft was recovered by the USS Leonard F. Mason.


GTA-8 
 

DateTimeEventOrbit  

1966 Mar 16  1641:02  Launch  
  T+0:41 3 km  -6368 x 4 x 28.5  
  T+1:10 10.0 km -6356 x 15 x 28.5 
  T+2:00 35.4 km -6247 x 60 x 29.0 
  T+2:14 46.1 km -6157 x 81 x 29.0 
 1643:35  T+2:33 BECO 
 1643:35  T+2:33 Stage 1 sep 62.6km -5924 x 124 x 29.5 
  T+3:20 104.1 km -5672 x 145  
  T+4:26 145 km  -4818 x 160  
  T+5:00 156 km  -3741 x 163 
  T+5:34 160.5 km  -542 x 160  
 1646:39  T+5:37 SECO  159 x 202 x 29.3  
 1646:44  T+5:42 Orbit insertion 
 1647:07  T+6:05 Stage 2 sep  160 x 285 x 29.0 
 1647:07  T+6:05 IVAR burn  161 x 270 x 28.91 
 1647:13  T+6:11 IVAR OAMS off 
 1648  T+7:35 Radar and horizon fairings jettison 
 1815:46  T+1:34:44 Lower apogee 5s 1m/s 
 1859:36  Phase Adj 15m/s 1:07  211 x 270 x 28.91 
 1926:52  Plane change (0.05deg) 35s 8m/s 
 1944:43  Vernier HAdj 0.6m/s 
 2029  Coelliptic NSR 19m/s 1:22  261 x 270 x 28.86 
 2121  Tally ho Agena 
 2155:56  TPI 10m/s 
 2208:25  MC burn 
 2220:22  MC 
 2224:11  TPF braking  
 2229  1 km from Agena 
 2237  Rendezvous with Agena 5003 at 46m 
 2314:18  Docking with Agena 5003 
 2314:24  Hard dock 
 2340  Thruster problem 
 2356:15  Undocked 
 2356  Sep burn from Agena 
 2358  Contact with CSQ 
1966 Mar 17  0000  Spin recovery  
 0006  Stabilized 
 0018Abort declared 
 0244:50  Adapter module sep  291.7 x 298.7 x 29.02 
 0245:48  Retro-1 fire over S China, 89m/s aft 35 down 
 0245:54  Retro-3 
 0245:59  Retro-2 
 0246:05  Retro-4 
 0246?  Retro module sep  9 x 314 x 28.85 
 0246?  Docking bar jettison 
 0307:48?  Entry  6 x 309  
 0322:28  Splashdown in E Pacific 
 0638  Recovered by USS Mason 

Satcom 3R

 1981-114A


RCA Americom replaced the Satcom 3 satellite with the first of a new Satcom series, 3R (RCA-D). 3R was used mostly for cable TV relay. The launch profile of the Delta 3910/PAM included a second stage single burn on a suborbital trajectory, with PAM-D ignition on the downward coast performing orbit insertion.

One source indicates this satellite and its successors may have released into the GEO band one or two cables used to carry structural loads during launch and then jettisoned after apogee firing.


Satcom 3R 
 

DateTimeEventOrbit  

1981 Nov 20  0137:31  Launch by Delta 3910  CC LC17A 
  T+0:57 SRM 1-6 burnout 
  T+1:00 SRM 7-9 burn 
  T+1:18 SRM 1-6 sep 
  T+1:58 SRM 7-9 burnout 
  T+2:03 SRM 7-9 sep 
  T+3:46 MECO  -4200 x 200?  
  T+3:54 St 1 sep 
  T+3:59 St 2 SES-1 
 0141 T+4:04 Fairing 
 0146 T+9:05 SECO-1  -795 x 283 x 27.2 
  Apogee 280 km 
 0157 T+20:12 St 2 sep 
 0158 T+20:54 PAM St 3 burn 
 0159 T+22:19 PAM burnout 
1981 Nov 20  0201:45  T+24:14 PAM-D sep  185 x 35809 x 27.5  
1981 Nov 20    627.60 193 x 35614 x 27.5 
1981 Nov 22  2230 AKM Star 30  GEO 138W 
1981 Nov 22    1418.75 35161 x 35731 x 0.8 GEO 138.7W+4.4E 
1981 Nov 25    1424.31 35266 x 35844 x 0.8 GEO 126.3W+2.9E 
1981 Dec 11    1427.92 35463 x 35788 x 0.4 GEO 108.8W2.0E 
1981 Dec 24   mv in 1436.08 35778 x 35793 x 0.1 GEO 131.0W 
1985 Mar 31    1436.14 35775 x 35799 x 0.0 GEO 131.0W 
1989 Mar 15    1436.14 35772 x 35802 x 0.1 GEO 131.1W 
1991 Jan 23    1436.05 35777 x 35794 x 0.1 GEO 131.0W 
1991 Apr 6  1436.07 35776 x 35797 x 0.3 GEO 130.8W 
1991 Apr 10   orbit raise 
1991 May 29    1438.28 35818 x 35839 x 0.4 GEO 158.2W+0.55W 

Thursday, July 4, 1991

Satcom 2

  1976-029A


The second satellite built by RCA Astro-Electronics for RCA Americom, RCA B (Satcom 2), was launched by Delta 3914 in Mar 1976.


Satcom 2 
 

DateTimeEventOrbit  

1976 Mar 26  2247  Launch by Delta 3914  CC LC17 
  T+0:57 SRM 1-5 burnout 
  T+1:04 SRM 1-5 sep 
  T+1:04 SRM 6-9 burn 
  T+2:07 SRM 6-9 sep 
  T+3:47 MECO 
  T+3:53 VECO 
  T+3:55 Stage 1 sep 
 2251 T+4:00 SES-1 
  T+4:25 Fairing sep
 2255 T+8:17 SECO-1  185 x 198 x 28  
 2307 T+20:35 SES-2 
 2308 T+21:16 SECO-2  185 x 1990 x 28 
 2309 T+22:08 St 2 sep 
 2309 T+22:49 St 3 burn 
 2310 T+23:33 St 3 burnout 
 2311 T+24:46 St 3 sep  185 x 35753 x 27.3  
1976 Mar 27  0500? Apo 1 85E 
 1530? Apo 2 70W 
1976 Mar 28  0200? Apo 3 130E 
 1230? Apo 4 30W 
 2230  Apo 5 180E 
1976 Mar 29  1000  Apo 6 12E 
 1930  Apo 7 138W 
1976 Mar 29  1930  AKM 8.9kN 35690 x 35883 x  
1976 Mar 31   Checkout GEO 128W 
1976 Jun 2   Replaced RCA 1 in commercial service GEO 119W 
1976 Aug   119W 
1976 Sep    GEO 119W 
1977 Jan 24    1436.07 35711 x 35861 x 0.0 GEO 119.1W 
1978 Jan 3    1436.07 35779 x 35793 x 0.0 GEO 119.0W 
1981 Jun    GEO 119.0W 
1982 Oct    GEO 119.0W 
1983 Apr 7    1436.08 35777 x 35795 x 0.0 GEO 119.0W 
1983 Apr 30   Partial solar array failure
1984 May    GEO 119W 
1984 May 27    1436.09 35779 x 35793 x 0.1 GEO 119.1W 
1984 May 29   Drift W  GEO dr 
1984 Jul 5    1436.23 35781 x 35796 x 0.2 GEO 139.0W 
1984 Jul    GEO 139W 
1985 Jan    GEO 139W 
1985 Jan 12    1436.02 35780 x 35789 x 0.4 GEO 138.6W 
1985 Jan 16 orbit raise1441.0 
1985 Jan 17   decommissioned 
1985 Jan 20   
1435.97 35779 x 35788 x 0.4 GEO 138.6W+0.02E 
1985 Feb 15    1460.06 35990 x 36518 x 0.5  
1986 Dec 9    1460.06 36001 x 36507 x 2.2 
1990 May 24    1460.10 36012 x 36498 x 5.5 
1995 Oct 12    1460.09 36025 x 36484 x 9.8 
1999 Apr 20    1460.09 36010 x 36499 x 11.7 

Seventeen: May 1991

 https://welib.org/md5/36b8b40d35b90a122343c0d7ab5b44be

Tuesday, July 2, 1991

Prospero

  1971-093A


The final Black Arrow launch from Woomera Site 5B, R-3, left the pad on 1971 Oct 28 carrying the X-3 technology satellite. X-3 was built and operated by the UK Royal Aircraft Establishment at Farnborough in Hampshire. X-3 and the Waxwing final stage motor reached polar orbit successfully. The 66 kg, 1.1m dia 0.71m high satellite was named Prospero. Prospero was still working in 1989 when the ground station at Lasham was closed down.

R-3 ussed Gamma 8 No 7 and Gamma 2 No 6.

Waxwing was 315 kg of prop at 156 kN. Dry mass was 35 kg; a 14 kg separation adapter was also orbited attached to Waxwing. One of Prospero's 0.5m aerials is believed to have been broken off shortly after separation.


Prospero 
 

DateTimeEventOrbit  

1971 Oct 28  0409:29 Launch by Black Arrow (R-3)  Woomera Site 5B 
 0411 T+2:06 Stage 1 MECO 
  T+2:13 St 1 sep 49 km  -6291 x 92  
 0411 T+2:13 Stage 2 burn 
  T+2:19 Interstage sep 
 0412 T+3:00 Fairing sep 93 km  -6166 x 147  
 0413 T+4:16 Stage 2 MECO 
  T+4:40 At 218 km, 23.48deg, 4.947 km/s 
  T+9:37 Stage 2 sep  -5036 x 552 x 80.38 
 0417 T+9:50 Stage 3 apogee burn 55s 
 0418  T+10:45 Stage 3 cutoff 
 0420 T+11:50 Stage 3 sep 
 0420 Prospero collides with stage 3 
   106.5 547 x 1582 x 82.1 
1989   Still operating

Kosmos 1793

 1986-091A


Plane 320 deg


Kosmos-1793 
 

DateTimeEventOrbit  

1986 Nov 20  1209:20 Launch by 8K78M  Plesetsk 
  BVGD sep 
  GO sep 
  T+4:46 Blok A sep 
  T+4:56 KhO sep 
  T+8:46 Blok-I MECO 
 1218 T+8:50 Blok-I sep 
  T+1:00? BOZ burn 
 1310?  T+1:00? BOZ sep 
  2BL burn 
  2BL MECO 
 1313?  T+1:03 2BL sep  
1986 Nov 20    (91B) 92.36 213x567x62.8 
1986 Nov 20    (91C) 183x613x62.9 
1986 Nov 20    (91D) 585x39191x63.0 
1986 Nov 20    578x39190x63.0 
1986 Nov 25    717.1 598x39748x63.0
1986 Nov 26    717.7 594x39755x63.0 

These Are Not My Beautiful Stories

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