Wednesday, August 21, 2002

Pioneer 7

  1966-075A


Pioneer B was launched at 1520:17 on 1966 Aug 17 by Delta E1 from Kennedy. The Delta separated at 1544:53 and the FW4 ignited at 1545:37. SP-278 and SP-280 give inconsistent values for the injection azimith corresponding to orbit inclinations of 22 and 42 deg respectively, with TR-1022 confirming the 42 deg value. Pioneer VII malfunctioned in 1972 Jul while at aphelion and lost some power, but it was still operable in 1980. 


Pioneer 7 
 

DateTimeEventOrbit  

1966 Aug 17  1520:17  Launch by Delta E1  CK LC17A 
  T+0:42 SRM burnout 
  T+1:11 SRM sep 
 1522:45  T+2:28 Thor MECO 95 km  -5522 x 188  
 1522  T+2:32 Delta burn 6:15 
  T+2:33 Thor sep 
  T+2:54 Fairing 
 1529:04  T+8:47 Delta SECO  
 1544:53  T+24:36 Delta sep  97.4 254 x 1022 x 33.00 
 1545:37  FW4D burn, 30.8s 
 1546:09  FW4D cutoff  367 x +Inf x 41.9 
 1547:09? FW4D sep 
  Delta orbit  97.04 252 x 994 x 32.8 
1966 Aug 26?   Solar orbit  
1966 Sep 25   In geotail at 1000 Re 
1966 Sep 26   XYZ(SE) = -900, 55, 22 
1966 Sep 28   XYZ(SE) = -950, 85, 25 
1966 Sep 30   XYZ(SE) = -1000, 130, 28 
1972 Jul   Electrical system malfunction 
1980   Still operational 

Opera: May 2002

 https://welib.org/md5/7b2c7f61a064a8870bcb31f2c5e34453

Us Weekly: March 18,2002

 https://welib.org/md5/3264713601d97dbd38256728dae70b79

Molniya 319

 1982-083A


Molniya-3 (F21, N19) was launched in Aug 1982 into plane A. It originally failed to make any burns to stabilize its ground track, but in mid September it started a series of small burns and later that month it was on station to replace F15 (N13). It reportedly carried an experimental SHF transponder.


Molniya-3 No. 33 
 

DateTimeEventOrbit  

1982 Aug 27  0002 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 
 0010 T+8:50 Blok-I sep  
  T+53:16 BOZ burn 
 0055  T+53:56 BOZ sep 
  ML burn 
  T+56:46 ML MECO 
 0058  T+56:54 ML sep   
1982 Aug 29  736.6 450 x 40827 x 62.9 
1982 Sep 15   Begin TCM burns 
1982 Nov 11  717.8 498 x 39856 x 62.9 
1987 Apr 2   end of ops 
2002 Jan 18 Reentered 

My Perfect Guy

https://welib.org/md5/8279c94536461c5f68e7412337027c33

MARECS 2

 1984-114B


INMARSAT's second successful MARECS, leased from ESA, was launched in Nov 1984. The 1050 kg ECS-bus satellite was built by British Aerospace.


MARECS 2 
 

DateTimeEventOrbit  

1984 Nov 10  0114:18  Launch by Ariane 3 (V11)  CSG 
  T+0:32 PAP sep 
  T+2:15 St 1 MECO 
  T+2:20 St 1 sep 
  T+2:20 Stage 2 burn 
  T+3:39 Fairing sep 
  T+4:24 St 2 MECO 
  T+4:29 St 2 sep 
  T+4:32 Stage 3 burn 
  T+4:43 St 3 ullage motors sep 
 0130:50 T+16:32 St 3 MECO 
  T+17:36 St 3 spinup 
  T+17:51 St 3 spindown 
 0132:41 T+18:23 Spacenet 2 sep from Sylda 4400 
 0133:44 T+19:26 Sylda sep 
 0135:21 T+21:03 MARECS 2 sep 
1984 Nov 11  0324:33 Mage burn 43s 
  Despin, uses 33 kg of hydrazine 
  Solar array deploy 
1984 Nov 11    1434.79 35606 x 35916 x 3.2 GEO 135.5E+0.3E 
1984 Nov 13    1431.51 35600 x 35793 x 3.1 GEO 136.2E+1.1E 
1984 Nov 16   Comms payload on 
1984 Dec 9    1431.77 35634 x 35769 x 3.1 GEO 165.1E+1.1E 
1984 Dec 19   Braking 
1984 Dec 21   mv in 1436.33 35782 x 35800 x 3.0 GEO 177.5E 
1985 Jan 8   Operational, POR Spare  GEO 177.5E 
1986 Jan 14    1436.07 35773 x 35799 x 2.4 GEO 177.5E 
1986 Jan 15   Traffic to MCS-D 
1986 Jan 15   mv out  GEO 177.5E dr 
1986 Feb 15    1456.60 36178 x 36195 x 2.3 GEO 17.8E+5.1W 
1986 Feb 25   AOR Primary, replaced MARECS 1  GEO 26W 
1986 Mar 2    1436.08 35769 x 35802 x 2.3 GEO 25.9W 
1987 Sep 25    1436.11 35774 x 35799 x 1.9 GEO 26.0W 
1989 Sep 7    1436.04 35772 x 35798 x 3.0 GEO 26.0W 
1990 Aug 31    1436.11 35775 x 35798 x 3.2 GEO 26.1W 
1990 Sep 19    1436.15 35773 x 35802 x 2.2 GEO 25.9W+0.02W 
1990 Nov   Moved to make new region 
1990 Nov 11    1436.16 35776 x 35799 x 1.7 GEO 55.4W+0.02W 
1990 Nov 19    1436.09 35774 x 35798 x 1.7 GEO 55.3W 
1992 Jun 26    1436.08 35774 x 35798 x 3.1 GEO 55.4W 
1992 Jul 7   mv out 1432.16 35689 x 35729 x 3.1 GEO 43.6W+0.9E 
1992 Aug 11   mv in  
1992 Sep 2    1436.07 35774 x 35798 x 3.2 GEO 15.1W 
1993 Mar 21    1436.09 35765 x 35807 x 3.7 GEO 15.0W 
1996 Mar 15    1436.10 35770 x 35803 x 6.0 GEO 15.0W 
1997 Jan 30    1436.13 35764 x 35810 x 6.6 GEO 15.5W 
1997 Feb   Move to 26W 
1997 Feb 20    1436.05 35771 x 35800 x 6.7 GEO 25.9W 
1999 May 17    1436.15 35769 x 35805 x 8.1 GEO 26.1W 
2002 Jan 18    1436.11 35769 x 35803 x 9.60 GEO 26.3W

Club Management: April 2002

 https://welib.org/md5/dba9a2c95fa1f47f5a8660133ed6c36a

Sunday, August 18, 2002

Raduga 32

 1994-087A


Raduga (Gran' 11F638) No. 43, Raduga (F33, N32), was launched on 1994 Dec 28. It operated until late 2000 or early 2001.


Raduga 43L 
 

DateTimeEventOrbit  

1994 Dec 28  1131  Launch by Proton-K  KB LC81 
 1140  Stage 3 sep 
 1240?  DM burn 1 
 1750?  DM burn 2 
 1810?  DM sep 
   1438.13 35740 x 35912 x 2.0 GEO 90.1E 
1995 Jan 1    1439.23 35787 x 35906 x 1.5 GEO 87.1E+0.8W 
1995 Jan 16    1436.24 35784 x 35794 x 1.4 GEO 70.6E 
1995 Mar 5    1436.21 35784 x 35792 x 1.4 GEO 69.0E 
1996 May 11    1435.99 35777 x 35791 x 0.5 GEO 71.0E 
1999 Oct 17    1436.07 35777 x 35794 x 2.1 GEO 70.1E 
2000 Nov 24    1436.00 35777 x 35791 x 3.0 GEO 70.9E 

Koronas-I

 1994-014A


A new generation of AUOS satellites, the AUOS-SM, was introduced by Koronas-I, the first science satellite launched by the Russian Space Agency. KORONAS is an acronym for Kompleksnie Orbital'nie Okolozemnie Nablyudeniya Aktivnosti Solntsa (Near Earth Orbital Complex for Studying Solar Activity). The I stands for IZMIRAN (Institut Zemnovo Magnetizma, Ionosferi i rasprostraneniya radiovoln AN Rossii), the terrestrial magnetism and ionospheric research institute of the Russian Academy Of Sciences. Koronas had the prelaunch designation AUOS-SM-KI-IK ( AUOS-SM-KI-IK) No. 801. The satellite was a 2298 kg 3-axis stabilized cylinder with solar panels. It was 5.0 m high and 2.3m in diameter, with a span of 12.8m once deployed. The satellite achived 40 arcsecond pointing (only 10 arcmin was required).


Koronas-I 
 

DateTimeEventOrbit  

1994 Mar 2  0325  Launch by 11K68 Tsiklon-3  NIIP-53 LC32 
 0327:00  T+2:00 Stage 1 sep (alt 48.1km) 
 0329:37  T+4:37 Stage 2 sep (alt 147.5 km) 
 0330:20  T+5:20 S5M burn 1 (alt 170.7 km) 
 0332:04  S5M MECO1 (alt 193.1 km, in transfer orbit)  170? x 507 x 82.5 
 0415:00  S5M burn 2 (alt 506.4 km) 
 0415:09  S5M MECO2 (alt 507.1 km) 
 0415:39  S5M sep  94.78 488 x 528 x 82.5 
1994 Jul?   lost attitude control 
1995 Apr   end of ops?
2001 Mar   Reentered 

Payload:

  • Terek Soft XR telescope-coronagraph spectroheliometer

November 20,2006

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