Friday, December 24, 2010

Insat 4B

 2007-007A


Insat 4B was an Ariane 5 payload similar to 4A. Mass 3028 kg launch 1335 kg dry, 3.1 x 1.8 x 2.0 m with 15.4m span. Mass 3029 kg launch 1325 kg dry according to EADS. Build by ISAC-Bangalore with 440N LAE.

In 2010 one solar array failed, reducing the satellite to half capacity.


Insat 4B 
 

DateTimeEventOrbit  

2007 Mar 11  2203 Launch by Ariane 5ECA 
  T+2:19 EAP sep 
  T+3:16 Fairing sep
 2211 T+8:58 EPC MECO 
 2212 T+9:04 EPC sep  -1251 x 157 x 7.22 
 2212 T+9:08 ESC-A MES 
 2227 T+24:47 ESC-A MECO 
 2229 T+26:40 Skynet 5A sep 
 2231 T+28:58 Sylda 5 sep 
 2234 T+31:02 Insat 4B sep 
2007 Mar 21  1911   631.91 246 x 35782 x 4.5 
2007 Mar 13   LAM  
2007 Mar 13  1605   921.83 14257 x 35737 x 1.2 
2007 Mar 14   LAM 
2007 Mar 15  0847   1361.11 32877 x 35734 x 0.2 
2007 Mar 16  0506  LAM 3:50   
2007 Mar 20    1432.31 35700 x 35724 x 0.2 GEO 55.5E+19.9E/d 
2007 Mar 23    1433.8 35703 x 35781 x 0.1 GEO 80.4E+0.6E/d 
2007 Apr 12   Arrive 93.5E 
2007 May 18    1436.2 35771 x 35804 x 0.1 GEO 93.5E 
2010 Jul 7   Solar array failure 

Poor Little Rich Girl

https://welib.org/md5/e4679a64f9396aa77c12d118a46328c6

Progress M-60

 2007-017A


11F615A55 No. 360 with a launch mass of 7264 kg. Flight 25P.

M-60 was used for the Plazma-Progress experiment,involving ground observations of plasma effects from Progress rocket burn.

 


PM60 
 

DateTimeEventOrbit  

2007 May 12  0325:38  Launch by Soyuz U Ts15000-104 (106)  KB 
 0334:27 T+8:49 Blok I sep 
 0715:23  DV1 22.0m/s 
 0759:23  DV2 5.1 m/s 
2007 May 14  0429:18  DV3 1.3m/s 
2007 May 15  0505  Braking  
 0509:57  Docked with Zvezda 
2007 Sep 19  0037:00 Undocked from Zvezda  91.30 331 x 344 x 51.6 
  Begin Plasma-Progress experiments 

2152  Burn 1, SKD, 1.5m/s 5s  91.25 331 x 340 x 51.6 
2007 Sep 20  1010   91.24 328 x 341 x 51.6 

2039:52  Burn 2, SKD, 6.3s 2.7m/s  91.22 325 x 343 x 51.6 
2007 Sep 21  2100:13  Burn 3, DPO 5s 2.6m/s retro 91.18 322 x 341 x 51.6 
2007 Sep 22  1944:59  Burn 4 SKD 6.3s 2.5m/s  91.16 320 x 343 x 51.6 
2007 Sep 23  2004:19  Burn 5, DPO 6.6s 1.6m/s  91.16 319 x 343 x 51.6 
2007 Sep 24  2023:25  Burn 6, DPO 5s, 1.1m/s posi  91.19 320 x 345 x 51.6 
2007 Sep 25  1901:00  Deorbited, 147s SKD, 84.2m/s 
 1903:27 SKD burn end 54 x 324 x 51.6 (dV) 
 1936:42  Entry interface 
 1948?  Impact Pacific 

Thursday, December 23, 2010

Soyuz TMA-3 (Inguli)

 2003-047A


The TMA-3 crew comprised MKS-8, the 8th main expedition, and EP-5, the 5th visting expedition, on mission ISS 7S.

Mike Foale is TMA-3 BI-2 and ISS Commander and Science Officer. Aleksandr Kaleri is TMA-3 Kdr and ISS flight engineer. Callsign was Ingul'. Pedro Duque is TMA-3 BI-1 and EP-5 ("Cervantes") crewmember.

Launch by Soyuz-FG; spacecraft 213. Callsign Inguli. Mass 7270 kg.

The Soyuz TMA-3 spaceship landed in Kazakhstan on Apr 30, returning the Expedition 8 and ESA DELTA crews to Earth. Mike Foale, Aleksandr Kaleri and Andre Kuipers entered TMA-3 from the Station's Pirs module and closed the hatches at 1747 UTC on Apr 29. They undocked from Pirs at 2052 UTC and fired their deorbit engines at 2320 UTC. The 115 m/s burn near apogee lasted 4min 23s and lowered the orbit from 354 x 371 km to about -32 x 369 km. The orbital and propulsion modules were jettisoned at 2345 UTC, and the descent module landed at 50 38N 67 20E around 0012 UTC on Apr 30, 55 km NE of Arkalyk.


Soyuz TMA-3 
 

DateTimeEventOrbit  

2003 Oct 18  0538:03  Launch by Soyuz-FG 
  T+1:53 SAS jettison 
  T+1:57 Strapons sep 
  T+2:37 Fairing sep 
  T+4:47 Blok A sep 
  T+4:57 KhO sep 
 0546:48 T+8:45 Blok I MECO 
 0546:51 T+8:48 Blok I sep7 88.58 190 x 218 x 51.65 
 0913:08  DV1 44s 17m/s 
 0950:55  DV2 43s 17m/s  89.90 266 x 272 x 51.6 
2003 Oct 19  0637:19  DV3 2m/s 6.2s  89.94 269 x 273 x 51.6 
2003 Oct 20  0504:47  DV4 42.1s 16.87m/s  
 0549:36  DV5 82.1s 33.69m/s  92.15 375 x 384 x 51.6 
 0638  Range 5 km 
 0645  Range 1.6 km 
 0650  Range 550m 
 0655  Begin flyaround 
 0703  Stationkeeping at 120m? 
 0708  Resume approach 
 0709  Range 107m 
 0710  Range 80m 
 0711  Range 50m 
 0714  Range 10m 
 0715:58  Docked with Pirs 
 0729  Hard dock 
 1019  HO to Pirs  92.15 375 x 384 x 51.6 
2004 Apr 29  1747  HC to Pirs 
 2052:09  Undock 
 2320:04  DO 4:23 115.2m/s 354 x 371 x 51.6 
 2324:19  DO CO  -32 x 369 x 51.6 
 2345:36  Modules sep 
 2348:19  Entry interface at 101 km 
 2354  End of blackout 
 2357  Parachute deployed
2004 Apr 30  0011:15  Landed

Aviation Week: August 23-30,2010

 https://welib.org/md5/5302a1542264454d15643b42c9736392

Raduga 2004

 2004-010A


The Globus satellite launched in Mar 2004 was originally named Kosmos-2406, but was redesignated Raduga-1 in May 2004.


Kosmos-2406/Raduga-1 
 

DateTimeEventOrbit  

2004 Mar 27  0330  Launch by Proton-K  KB LC81 
  T+2:06 St 1 sep 
  T+3:03 GO sep 
  T+5:30 St 2 sep 
  T+9:34 St 3 MECO 
 0339  T+9:44 Stage 3 sep 
 0443 T+1:13:25 Blok DM-2 MES-1 
 0450 T+1:20:28 DM MECO-1  x 49.2  
 1000 T+6:33:49? SOZ burn 
 1000 T+6:33:49 DM MES-2 
 1004 T+6:37:02 DM MECO-2 
 1006  DM sep 
2004 Apr 21    1436.01 35772 x 35797 x 1.4 GEO 85.0E 
2004 May 18   DM orbit  1438.60 35498 x 36172 x 1.3 
2006 Aug 8    1436.07 35777 x 35794 x 1.3 GEO 85.4E 
2010 Feb 5    1435.40 35757 x 35788 x 4.4 GEO 85.0E 

Tuesday, December 21, 2010

Progress M-56

 2006-013A


11F615A55 No. 356. Launched by 11A511U-PBV P15000-100. Mission 21P to dock with Zvezda. Mass 7281 kg.


Progress M-56 
 

DateTimeEventOrbit  

2006 Apr 24  1603:25 Launch by Soyuz-U  KB LC1 
  T+1:59 Strapons sep 
  T+2:41 GO sep 
  T+4:47 Blok A sep 
  T+4:57 KhO sep 
  T+8:46 Blok I MECO 
 1612:14 T+8:49 Blok I sep 
 1938s  DV1 
 2029s  DV2 
2006 Apr 25  1709  DV3 
2006 Apr 26  1703Braking 
 1720Flyaround begins at 400m 
 1731  Stationkeep at 160m 
 1732  Final approach  

1741:31  Docked with Zvezda 
2006 May 4  1129  Orbit raise 393s burn 
2006 Aug 23 1604 PM56 orbit raise 
2006 Sep 19  0028:17  Undocked 
 0031  Sep burn 
 0328:00  Deorbit 162.9s 85.3 m/s  334 x 349 x 51.6 
 0330:43 Deorbit CO55 x 338 x 51.6 
 0403:44 Entry 

Escaping the Bonds of Earth: The Fifties and the Sixties

 https://welib.org/md5/90431d9f3565efd59187ea0206687521

NATO 4B

 1993-076A


NATO IVB was launched in Dec 1993. After two months slow drift across the Atlantic, it was placed on station in early Mar 1994 over 6E. In 1998 it was moved to the 20W position.


NATO IVB 
 

DateTimeEventOrbit  

1993 Dec 8  0048:00  Launch by Delta 7925  CC LC17 
  Az 95 deg 
  T+1:03 SRM 1-6 off 
  T+1:06 SRM 1-6 sep 
  T+2:09 SRM 7-9 off 
  T+2:12 SRM 7-9 sep 
  T+4:20? MECO 
  T+4:28 St 1 sep 
  T+4:34 Delta stage 2 burn 
 0059 T+11:03 Delta SECO-1  185? x 2119? x 29.4? 
   164? x 2119? x 29.4 
 0109 T+21:25 Delta SES-2 
 0109  Delta SECO-2  300? x 2119? x 29.4  
 0110  Delta sep 
 0111  TES 
 0112  TECO 
 0114  T+26 Stage 3 sep  643.70 725 x 35908 x 23.2  
 0142? SES-3 depletion  109.77 313 x 2119 x 23.0  

1993 Dec 10  

1239? Star 30E AKM 
1993 Dec 11    1448.20 35095 x 36951 x 4.2 GEO 14.7W+3.0W 
1994 Jan 9    1440.95 35117 x 36645 x 4.1 GEO 59.6W+1.2W 
1994 Mar 11   mv in  1436.20 35786 x 35790 x 3.8 GEO 5.9E 
1994 Jun 2    1436.06 35782 x 35789 x 3.9 GEO 6.0E 
1997 Jul 22    1436.07 35776 x 35795 x 2.3 GEO 6.0E 
1998 Jan 14   mv out 1436.20 35773 x 35803 x 2.1 GEO 5.8E 
1998 Feb 1    1438.54 35776 x 35892 x 2.1 GEO 6.1W+0.6W 
1998 Mar 28   mv in  1436.11 35776 x 35797 x 2.0 GEO 20.2W 
1999 Oct 17    1436.12 35772 x 35801 x 1.5 GEO 20.3W 
2006 Jul 10    1436.11 35772 x 35801 x 5.3 GEO 20.3W 
2006 Nov? Move out 
2007 Feb 4    1435.90 35777 x 35787 x 5.8 GEO 35.4E 
2008 Nov 25  1436.11 35774 x 35799 x 7.0 GEO 34.9E

May 13,2026

  https://planet4589.org/space/jsr/back/news.855.txt