Thursday, September 18, 1986

Corona 114

 1967-002A


KH-4A Mission 1038 was launched on 1967 Jan 14 by TAT Agena D from Vandenberg into an 80 degree orbit. Mission 1038-1 was completed on Jan 19 after 5 days, and Mission 1038-2 ran from Jan 19 to Jan 26 for a duration of 7 days. Both SRVs were recovered and the image quality was recorded as fair to poor, possibly due to atmospheric factors.


KH-4A Mission 1038 
 

DateTimeEventOrbit  

1967 Jan 14  2128:21 Launch by Thor SLV-2A Agena D  V SLC3W 
 2128:18  Launch (PerfER) 
 2129:17 Castor sep (T+0:56) 
 2130:51  Thor MECO (T+2:30)  
 2130:59  Thor VECO (T+2:38) 
 2131:05  Thor sep (T+2:44) 
 2131:11  Agena burn (T+2:50) 
 2136:14  Agena MECO (T+7:53)  90.18 185 x 390 x 80.00 (VCR)  
1967 Jan 14  2356   90.12 180 x 381 x 80.1 
1967 Jan 15  1327   90.08 177 x 379 x 80.1 
1967 Jan 15  1430  90.13 180 x 380 x 80.07 (RAE) 
1967 Jan 16  2230   90.05 178 x 375 x 80.08 
1967 Jan 19  2305? SRV-1 ejected rev 81 
 2331  Recovered midair (PerfR) 
1967 Jan 19  2343 SRV-1 recovered (PER) 
  26 03.0N 155 54.0W 
1967 Jan 20  1633   89.93 176 x 366 x 80.07 
1967 Jan 23  0600   89.82 175 x 356 x 80.1 
 2359   89.80 175 x 353 x 80.1 
1967 Jan 26  1620   89.68 172 x 338 x 80.1 
1967 Jan 26  2248? SRV-2 ejected rev 193 
1967 Jan 26  2327 SRV-2 recovered (PER) 
 2338  Recovered midar (PerfR) 
  23 43.0N 169 01.0W 
1967 Jan 28  0543   89.62 172 x 338 x 80.1 
1967 Feb 1  2238   88.13 146 x 217 x 80.1 
1967 Feb 2  1430?? CORONA/Agena reentered 

Tuesday, September 16, 1986

Corona 128

 1968-078A


KH-4A Mission 1048 was launched by Thorad Agena D from Vandenberg on 1968 Sep 18. Both SRVs were recovered but the forward camera failed on mission 1048-2 during pass 181D. The mission carried at least 7 DMU rockets, possibly of a modified design; the first was used as planned to achieve the nominal orbit; the next three were used to maintain orbital height; and the last three were fired retrograde and used to test out the Thiokol motors. DMU 6 and 7 were 3000 lb-s; the remaindeer were 2000 lb-s versions.


KH-4A Mission 1048 
 

DateTimeEventOrbit  

1968 Sep 18  2132  Launch by LTTAT Agena D  
 2131  Launch (PerfER) 
 2133 Castor sep 
 2135 Thor sep 
 2136 Agena burn 
 2140 Agena MECO 
 2306? Subsatellite ejected 
1968 Sep 18  2059   90.11 166 x 393 x 83.0 
  DMU burn 1 rev 4 
1968 Sep 19  1632   90.16 175 x 389 x 83.0 
1968 Sep 19   90.12 167 x 393 x 83.0 (RAE) 
1968 Sep 20  0604   90.17 182 x 383 x 83.0 
1968 Sep 22   DMU burn 2 rev 56 
1968 Sep 25  0023   90.19 177 x 390 x 83.0 
1968 Sep 27  1532   90.10 176 x 382 x 83.0 
1968 Sep 27   DMU burn 3 rev 136 
 2331? SRV-1 ejected 
1968 Sep 28  0010 SRV-1 recovered rev 145; 23 38N 169 07W 
 0015  SRV-1 recovered (PerfR) 23 38 N 169 07 W 
1968 Sep 30    90.1 178 x 391 x 83.0 (SSR) 
1968 Oct 2  2224?  SRV-2 ejected rev 224 
1968 Oct 2  2305  SRV-2 recovered 17 34N 160 49W 
1968 Oct 2  2330?  DMU burn 4 rev 225 
1968 Oct 3   DMU burn 5 rev 229, retro 6m/s 
1968 Oct 3  0951   89.49 168 x 331 x 83.1 
  DMU burn 6 rev 233, retro 9m/s 
1968 Oct 3   DMU burn 7 rev 238, retro 9m/s 
1968 Oct 5  2258   88.91 167 x 274 x 83.0 
1968 Oct 8   Reentered 

Tuesday, September 2, 1986

Kosmos 1304

 1981-087A




Kosmos-1304 
 

DateTimeEventOrbit  

1981 Sep 4  1106  Launch by Kosmos-3M  PL LC132 
  T+2:10 St 1 MECO 
  T+2:12 St 1 sep 
  T+2:12 St 2 burn 59km 
  T+2:27 Fairing sep 76km 
 1114?  T+8:03 St 2 MECO 150 km  150 x 1003? x 83 
  T+1:02:19 St 2 MES2 
  T+1:02:30 St 2 MECO2 
 1209?  T+1:02:50 St 2 sep 

 
1981 Sep 4   103.99 911x978x82.94 

Sunday, August 24, 1986

Kosmos 1300

 1981-082A


With Kosmos-1300, launch of the Tselina-D satellites began to switch to the Tsiklon-3 launch vehicle.


Kosmos-1300 
 

DateTimeEventOrbit  

1981 Aug 24  2140 Launch by 11K68  Plesetsk 
  T+2:00 St 1 sep 
  T+3:33? GO sep 
  T+4:38? St 2 sep 
  T+5:20? S5M burn 1 
 2146 T+6:48 S5M MECO1 km 60? x 650 x 82.5 
  T+40:58? S5M burn 2  
  T+41:08? S5M MECO2 
 2221 T+41:38? S5M sep 
1981 Aug 24    97.8 638x702x82.5 

Transtage 1

 1964-081A


The second launch was Titan IIIA-1, which orbited Transtage 1 with a 1366 kg payload. (ETR report says 1700 kg lead payload; MR641221-8 says 1524 kg, but the 1968 Transtage flight summary seems definitive.) In this case the truss was 148 kg with 1218 kg of ballast.


Transtage 1 
 

DateTimeEventOrbit  

1964 Dec 10  1653:33  Launch by Titan IIIA  CK LC20 
 1655?  St 1 sep 
 1659?  St 2 sep 
 1659?  Transtage MES-1 
 1705?  Transtage MECO-1 
   87.60 157 x 170 x 32.15 
1964 Dec 13  0940Reentered over Argentina 

Friday, August 22, 1986

Interkosmos 3

 1970-057A


The first DS-U2-IK Interkosmos ionospheric payload, Interkosmos-3, was launched on 1970 Aug 7 by 11K63 from Kapustin Yar. It studied high energy trapped protons and electrons, and propagation of radio waves in the ionosphere. 


Interkosmos-3 
 

DateTimeEventOrbit  

1970 Aug 7  0300  Launch by 11K63 Kosmos-2  GTsP4 
 0302  S1 burn 
 0310? S1 sep 
   99.7 200 x 1295 x 48.4 
1970 Dec 4   end of ops 
1973 Feb 12 reentered

Payload:

  • PG-1 Particle detectors (high energy protons, electrons)

  • ANCh-1 Ionospheric VLF receiver

  • UKV-4M Short wave radio beacon

Monday, August 11, 1986

Kosmos 396

 1971-014A


This February 1971 Zenit-4M launch was a 13 day flight from Plesetsk at 65.4 deg. An orbit raise burn was made around Feb 24.


Kosmos-396 
 

DateTimeEventOrbit  

1971 Feb 18  1359:59  Launch by 11A57  PL 
 1404  Blok-I burn  
 1408  Blok-I sep  
 1644   89.43 207 x 285 x 65.4 
1971 Feb 20  1029   89.39 204 x 284 x 65.4 
1971 Feb 210930   89.40 205 x 286 x 65.42 (RAE) 
1971 Feb 23  1247   89.05 187 x 267 x 65.4 
  Orbit raise 
1971 Feb 25  1900   89.30 189 x 292 x 65.42 (RAE) 
1971 Feb 28  0246   89.23 185 x 287 x 65.4 
1971 Mar 3  0630?  Engine sep (14E) 

0633? Deorbit  
 0643? PO sep 
 0649? Entry 
 0703?  Landed 

Thursday, August 7, 1986

Intelsat 509

 1984-057A


The last MCS satellite, Intelsat V F-9, was stranded in low orbit when its Centaur stage failed. A clogged fuel line meant that the first burn was 8 seconds shorter than planned, and the second burn shut down only 3.5 seconds into a planned 91 second firing. The thrusters were used to raise the orbit slightly; the satellite was deorbited using the apogee motor after 138 days. Following the loss of the Westar and Palapa satellites earlier in the year, the Intelsat failure triggered a rise in insurance premiums.


Intelsat V F-9 (MCS) 
 

DateTimeEventOrbit  

1984 Jun 9  2303:00  Launch by Atlas G Centaur  CC LC36 
  T+2:10? BECO 
  T+2:13 Booster sep 
  T+2:44 Centaur insulation sep 
  T+3:29 Fairing sep
  T+4:14 MECO 
  T+4:17 Atlas sep  
  T+4:23 Centaur MES1 
 2312:26  T+9:26 Centaur MECO1 (8 s short)  172 x 318 x 28.7 
 2326:42  T+23:42 Centaur MES2  
 2326:45  Centaur MECO2 (after 3.5s)  187 x 1240 x 29.2 
 2329?  T+26:36 Centaur sep 
1984 Jun 10    98.77 176 x 1222 x 29.2 
1984 Jun 11    98.69 172 x 1219 x 29.1 
1984 Jun 16 
99.31 229 x 1221 x 28.7 
1984 Jul 19    99.05 238 x 1187 x 28.7 
1984 Oct 22   98.29 242 x 1111 x 28.7 
1984 Oct 24  0910?Star 37XF fired to deorbit 

0955?Reentered 

Friday, August 1, 1986

Corona 89

  1964-075A


KH-4A Mission 1014 was launched on 1964 Nov 18 by Thrust Augmented Thor Agena D from Vandenberg into a 70 degree orbit for coverage of Cuba. The cameras operated successfully and both SRVs were successfully recovered. CORONA 89 also carried the USAF Cambridge Research Labs (AFCRL) ORBIS ionospheric beacon, which extended a 7.5 meter antenna transmitting at 10 MHz (there were also 5 and 0.19 MHz beacons which failed to operate). Launch was 4 hours earlier than normal to provide coverage of `certain areas' at times of long shadows. The mission carried an experimental filter set and smaller slits and included imagery of the Balkans and Zaire.


KH-4A Mission 1014 
 

DateTimeEventOrbit  

1964 Nov 18  2035:54  Launch by TAT Agena D  
 2036:59  Castor sep (T+1:05) 
 2038:26  Thor MECO (T+2:32) 
 2038:35  Thor VECO (T+2:41) 
 2038:42  Thor sep (T+2:48) 
 2038:47  Agena burn (T+2:53) 
 2042:50  Agena MECO (T+6:56)  89.77 189 x 369 x 70.04 (VCR) 
1964 Nov 19  0932   89.70 182 x 336 x 70.0 
1964 Nov 20  0030   89.71 176 x 344 x 70.0 
1964 Nov 21  0754   89.69 177 x 340 x 70.0 
1964 Nov 21  1700   89.71 180 x 339 x 70.02 
1964 Nov 23 2140? SRV-1 ejected rev 81 
1964 Nov 23 2217 SRV-1 recovered 
1964 Nov 24  0739   89.62 176 x 335 x 70.0 
1964 Nov 27  1916   89.52 175 x 327 x 70.0 
1964 Nov 27 2115?  SRV-2 ejected rev 145 
1964 Nov 27 2151 SRV-2 recovered  
1964 Nov 30  0657   89.44 177 x 316 x 70.0 
1964 Dec 1   End of transmissions 
1964 Dec 3  0450   88.93 167 x 276 x 70.0 
1964 Dec 6   Reentered after 17.45d 

Thursday, July 31, 1986

Kosmos 1075

 1979-010A


Fourth low orbit launch.


Kosmos-1075 
 

DateTimeEventOrbit  

1979 Feb 8  1000 Launch by 11K65M  Plesetsk 
 1020?  Stage 2 sep 
1979 Feb 8    94.5 473x516x65.8 

November 20,2006

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