Saturday, March 2, 1985

Ferret 15

 1970-066A


The third STRAWMAN carried the standard THRESHER and REAPER payloads only, on mission 7166.

REAPER was able to locate radars to 7 km accuracy.


OPS 8329 
 

DateTimeEventOrbit  

1970 Aug 26  1001 Launch by LTTA Thor Agena D  
 1002? Castor II SRMs sep (T+1:42?) 
 1004?  Thor MECO (T+3:37?) 
 1004? Thor VECO (T+3:46?) 
 1004?  Thor sep (T+3:52?) 
 1004?  Agena burn (T+3:58?) 
 1009?  Agena MECO (T+8:00?)  -100? x 483 x 75.0 
 1031? Agena MES-2 
 1031? Agena MECO-2 
1970 Aug 27  0903   94.48 484 x 501 x 75.0 
1970 Dec 12   THRESHER TI mode failed 
1971 Jan 16    94.27 474 x 491 x 75.0

Monday, February 18, 1985

Venera 5

  1969-001A


V-69 No. 330 was named Venera-5 after its successful launch. The solar orbit insertion burn was over Africa. The SA stopped transmitting at an altitude of 25 km. It impacted at -3 latitude, 18 longitude. Conditions at the site were calculated to be 530 C, 140 bar.


Venera-5 
 

DateTimeEventOrbit  

1969 Jan 5  0628  Launch by 8K78M  KB 
 0633  Blok-A sep 
 0633  Blok-I burn 
 0637  Blok-I sep 
 0747  BOZ burn 
1969 Jan 5  0747  Blok-L burn 3:48, solar orbit 
 0751  Blok-L sep 
 1000  25100 km over SE China 
1969 Mar 3   TCM 9m/s 
1969 May 16  0408  Landing sequence on at range 50000 km 

0436SA sep, range 37000 km 
 0601  Entry 11.16km/s 
 0602:30  AOS, parachutes out 
 0654:56  End of signal, 53 min, 25 km up 
 0715?Impact  

Surveyor 7

  1968-001A


Surveyor SC7 (Surveyor G) was launched at 0630:01, on azimuth 102.9 deg, on 1968 Jan 7 by Atlas Centaur. The Centaur coasted in parking orbit, then reignited and shut down at 0705:16 to deliver Surveyor VII to a translunar trajectory. The Surveyor made a course correction at 2230 on 1968 Jan 7. The radar was jettisoned around 0100 on Jan 10 and the retro fired successfully, with landing at 0105:38 on Jan 10 on the Tycho ejecta blanket. For the first time both the alpha-scatter and sampler experiments were carried on the same mission. The craft returned over 21000 pictures, and survived one lunar night. The surface sampler was tested, manipulating rocks and digging trenches. On the second lunar day, battery degradation limited operations. The last transmission from Surveyor VII was at 0024 on 1968 Feb 21. 


Surveyor 7 
 

DateTimeEventOrbit  

1968 Jan 7  0630:01  Launch by Atlas SLV-3C Centaur  CC LC36 
 0632:33  BECO  
 0632:36  Booster sep-5940 x 100 ? 
 0633:17  Insulation panels jettison 
 0633:47  Fairing 
 0634:09  Atlas SECO  -5450 ? x 166 ? 
 0634:11  Atlas sep 
 0634:21  Centaur MES-1 
 0639:53 Centaur MECO-1  87.80 166 x 176 x 30.69 
  22.5 min coast 
 0702:20 Centaur MES-2  
 0704:15  Centaur MECO-2 166 x 729739 x 30.68 (GD) 
 0704:33  SV legs deploy 
 0705:16 Centaur sep  169 x 697813 x 30.69 
 0709:16 Centaur retro  
 0713:25 Centaur retro complete 166 x 483702 x 30.68 (GD) 
 2330:09  MCC 11.3s 11.1m/s  217 x 716748 x 29.5 
1968 Jan 10  0035  Attitude for landing 
 0057:34  AMR on 
 0102:13  Vernier engines on 
1968 Jan 10  0102:14  Radar jettison  -1056 x -9282 x 62.85  
 0102:14 Retro 
 0102:57  Retro burnout 
 0103:08  Vernier high thrust 
 0103:09  Retro eject  -1736 x 18 x ? 
 0105:12  Altitude 300m 
 0105:28  Altitude 15m 
 0105:36  Landing 40.89S 11.44W 
 1326  AC-15 flyby 19743 km 
  Centaur orbit  167124 x 445181  
1968 Jan 26 1412 Shutdown for lunar night 
1968 Feb 12  1900 Revived for day 2 
1968 Feb 20   Communications problems 
1968 Feb 21  0024  Last transmission 

Sunday, February 10, 1985

Molniya 121

 1970-101A


Molniya-1 (F21,N16) entered the D plane, replacing N14 and being replaced by N22.


Molniya-1 F21 
 

DateTimeEventOrbit  

1970 Nov 27  1547:17 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 
 1555 T+8:50 Blok-I sep 
  T+53:16 BOZ burn 
 1640?  T+53:56 BOZ sep 
  ML burn 
  T+56:46 ML MECO 
 1643?  T+56:54 ML sep   
1970 Dec 6    707.15 469 x 39359 x 65.5 
1970 Dec 9    707.20 438 x 39393 x 65.5 
1970 Dec 22    717.81 462 x 39893 x 65.4 
1971 Apr 16    717.81 612 x 39743 x 65.5 
1971 Apr 24    717.78 624 x 39730 x 65.5 
1971 Jun 2    717.70 703 x 39647 x 65.5 
1972 Feb?   end of ops
1974 Aug 1    717.97 807 x 39556 x 65.6 
1975 Jul 24    717.51 202 x 40139 x 65.2 
1975 Nov 25   Reentered 

Friday, January 25, 1985

Ume 1

 1976-019A


NASDA and the Radio Research Lab (RRL) developed the Ionospheric Sounding Satellite (ISS), a 135 kg, 0.82 m long, 0.94m diameter spacecraft with a swept frequency topside sounder with 36.8m and 11.4m span dipole antennae covering a range from 0.5 to 148 MHz. Prime contractor was Mitsubishi. The satellite was named Ume (Japanese apricot blossom) after launch. Launch was southeast from TNSC at azimuth 115 deg (corresponding to a 38 deg inclination); a yaw burn in second stage changed inclination to 70 deg.


Ume 
 

DateTimeEventOrbit  

1976 Feb 29  0330  Launch N-I 2  TNSC 
 0333  St 1 sep  -6000? x 200? x 38?  
  Fairing sep
 0335  St 2 burn 4:30 
 0339  St 2 cutoff  -3200 x 998 x 51.4  
 0340  St 3 burn, circ 
 0341? St 3 sep  105.2 994 x 1013 x 69.7 
1976 Mar   Electrical malfunction 
1976 Aug 2   End of tx 

Payload:

  • TOP Swept frequency topside sounder, 36.8m., 11.4m dipoles; 0.5-148 MHz

  • PIC Ion mass spectrometers

Sunday, January 20, 1985

Contemporary Music Almanac: 1980-81

 https://welib.org/md5/0470d2a1e9f89a33c56525bb1a07c7eb

Space World: November 1984

 https://welib.org/md5/469478caaac8cbebb79609d0f5c241ad

Town and Country: August 1984

 https://welib.org/md5/394f62725142f6b1b2c97a674870a751

Molniya 103

  1965-030A


The third launch of an 11F67 Molniya-1, Molniya-1 No. 3, was the first to be given the Molniya-1 name.


Molniya-1 (F3) 
 

DateTimeEventOrbit  

1965 Apr 23  0155 Launch by 8K78  KB 
 0200?  Blok-A sep 
 0200? Blok-I burn 
 0204?  Blok-I sep 
 0255? BOZ burn 
 0256? Blok-L burn 
 0300? Blok-L sep 
1965 Apr 23  0321   94.38 198 x 778 x 64.8 
1965 Apr 25  0228   707.29 530 x 39305 x 65.5 
1965 Apr 29  0046   707.25 535 x 39298 x 65.1 
1965 Apr?   TCM, test of KDU 
1965 May 4    720.55 529 x 39961 x 65.3 
1965 Nov 26   End of operations 
1978 Oct 29    718.13 244 x 40127 x 64.2 
1979 Feb 22    668.98 151 x 37767 x 64.1 
1979 Apr 10    558.93 107 x 32089 x 64.1 
1979 May 8   Reentered 

Payload:

  • C-band 6/4 GHz transponders

November 20,2006

  https://en.wikipedia.org/wiki/Association_football