Thursday, January 28, 1982

Kosmos 695

 1974-091A


DS-P1-Yu No. 73 was launched in Nov 1974.


Kosmos-695 
 

DateTimeEventOrbit  

1974 Nov 20  1200  Launch by 11K63  NIIP-53 LC133/1 
 1202  Stage 2 burn 
 1206? Stage 2 sep 
1974 Nov 20    92.0 273 x 468 x 71.0 
1975 May 10   End of ops 
1975 Jul 15   Reentered 

Sunday, January 24, 1982

IDCSP 3

  1968-050A


The third and final IDCSP Initial Defense Communications Satellite Program cluster was launched by Titan IIIC on 1968 Jun 13. It had initially been planned as a replenishment launch but most of the previous IDCSP satellites were still operating well. The first satellite of the eight in the cluster was IDCSP 20,.


IDCSP 20 
 

DateTimeEventOrbit  

1968 Jun 13  1403:50  Launch by Titan IIIC (3C-16)  CC LC41 
  T+0:02:01 SRM sep 
  T+0:02? St 1 burn 
  T+0:04:17 St 1 sep 
  T+0:04:41 Fairing 
  T+0:07:38 Titan Stage 2 MECO   
 1411:41  T+7:51 Transtage burn 1 14s  
 1411:55  T+8:05 MECO-1 148 x 176 km x 28.6 
 1509:32  T+1:05:42 Transtage burn 2   
 1514:35 T+1:10:45 MECO-2  250 x 33700 x 26.4 
 2005 T+6:02:52 MES-3 
 2008 T+6:04:38 MECO-3 
 2010? IDCSP sep 
   1335.7 33758 x 33841 x 0.2 

Saturday, January 23, 1982

Molniya 207

  1973-076A


Molniya-2 F7 was launched on 1973 Oct 19 into a 62.8 degree orbit, the first Molniya-2 to enter such an orbit. It was located in the D plane.


Molniya-2 F7 
 

DateTimeEventOrbit  

1973 Oct 19  1026:01 Launch by 8K78M  PL 
  BVGD sep 
  GO sep 
  T+4:46 Blok A sep 
  T+4:56 KhO sep 
  T+8:46 Blok-I MECO 
 1034  T+8:50 Blok-I sep  
  T+53:16 BOZ burn 
 1119  T+53:56 BOZ sep 
  ML burn 
  T+56:46 ML MECO 
 1122  T+56:54 ML sep   
1973 Oct 19  1140  (approx?) 722.96 555 x 40055 x 62.9 
1973 Oct 22  1315   735.87 616 x 40626 x 62.8 
  Lower orbit 
1973 Oct 25  1415   717.94 502 x 39859 x 62.8 
1973 Dec 19  1016   717.81 608 x 39747 x 62.9 
1975 May 21    717.67 511 x 39837 x 63.8 
  Orbit raise 
1975 May 27    732.61 496 x 40587 x 63.9 
1975 Oct 3    732.58 488 x 40593 x 64.1 
1975 Oct 7   End of ops 
1978 Jan 19    732.63 1141 x 39943 x 65.0 
1983 May 23    687.25 111 x 38726 x 64.1 
1983 Jul 8   Reentered 

Tuesday, January 12, 1982

Kosmos 16

  1963-012A


Zenit-2 No. 10 was launched the day after the landing of Zenit-2 No. 8, the first time this had happened in the Zenit program. The spacecraft flew a 10 day mission, a record which would stand for five years. 


Kosmos-16 
 

DateTimeEventOrbit  

1963 Apr 28  0849:56  Launch by Vostok 8A92  KB 
 0855?  Blok-E burn 
 0859?  Blok-E sep  
   90.4 207 x 401 x 65 (TASS) 
   90.38 194 x 388 x 65.0 (RAE) 
1963 Apr 28    90.33 198 x 383 x 65.1 
1963 May 7    90.22 190 x 379 x 65.0 
1963 May 8  0630?  Retrofire 
1963 May 8  0650?  Landed after 9.9d 

Saturday, January 9, 1982

Molniya 107

  1966-092A


Molniya-1 No. 7 was the last OKB-1 built Molniya and the first to achieve a stabilized 12-hour period ground track, in Nov 1966. Improvements to the solar panels made it longer lived, operating for more than a year.


Molniya-1 7 
 

DateTimeEventOrbit  

1966 Oct 20  0750 Launch by 8K78M  KB 
 0754?  Blok-I 
 0759? Blok-I MECO 
 0850?  BOZ burn 
 0851?  Blok L burn 
 0855? Blok L sep 
1966 Nov 8    713.23 454 x 39675 x 64.6 
1966 Nov   Ground track stabilized 
1966 Dec 1    718.12 464 x 39907 x 64.7 
1967 Jan 27    717.87 480 x 39878 x 64.8 
1968 Jan 29  End of ops 
1968 Jul 3    712.48 181 x 39911 x 65.0 
1968 Sep 11   Reentered 

Friday, January 8, 1982

DSAP 2

 1965-072A


Vehicle 1 in the Block 2 series was orbited on 1965 Sep 10, using a Thor Burner 1 with an FW4 upper stage. It operated on its primary mission for 341 days. The satellite carried a 1.3cm video camera, the medium resolution `C' IR camera system with 16 sensors in the 0.2-5 micron band and the 5-30 micron bands, and a high resolution radiometer (HRR) in the 7-14 micron bands.


DSAP 01213 
 

DateTimeEventOrbit  

1965 Sep 10  0441:38  Launch by Thor Burner 1  V 4300B6 
 0444:16  Thor MECO (T+2:38) 
 0444:24  Thor VECO (T+2:46) 
 0444:35  Heatshield sep (T+2:57) 
 0452:03  FW4 spinup (T+10:25) 
 0452:04  Thor sep (T+10:26) 
 0452:10  FW4 burn (T+10:32) 
 0452:43  FW4 burnout (T+11:05) 
 0452  FW4 sep  
 1430  101.93 649 x 1054 x 98.7 (RAE) 
1966 Aug 17   end of primary mission 
1966 Sep 22   end of ops

Payload:

  • Video camera

  • System C IR camera

  • High resolution radiometer

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