Thursday, October 6, 2011

Haiyang 3

 2011-043A


Ocean No. 2 (Haiyang er hao) with CZ-4B. Orbit was 689 x 712 km x 88 deg.


HY2 
 

DateTimeEventOrbit  

2011 Aug 15  2257  Launch by CZ-4B  TYSC 
 2259?  St 1 sep 
 2300?  Fairing sep
 2303?  St 2 MECO 
 2303?  St 2 sep 
  St 3 burn 
 2307?  St 3 MECO 
 2317?  St 3 sep 

Payload:

  • MWI Microwave imager, for brightness temp

  • RA Dual band radar altimeter C/Ku, sea levels and wind speeds

Tuesday, October 4, 2011

Skynet 4D

 1998-002A


Skynet 4D is the first of three replacement Skynet 4 Stage 2 satellites. It will be launched 1998 by Delta. It is built by Matra Marconi Space/Stevenage. It still uses the old ECS bus, but has a steerable high power SHF spot beam and widebeam antennae.

During launch, the Delta second stage suffered two jolts, one during the second burn and one 15 s into the depletion burn, which caused the nearly empty stage to tumble.

The Skynet 4D was transferred from MMS to MoD on 1998 May 20.

In early 2003 4D was moved from the Atlantic position to support troops in the Middle East.


Skynet 4D 
 

DateTimeEventOrbit  

1998 Jan 10  0032:01  Launch by Delta 7925  CC LC17B 
 0033:04  SRM 1-6 burnout 
 0033:07  SRM 7-9 burn, 1-6 sep 
 0034:10  SRM 7-9 burnout, sep 
 0036:24  T+4:23 MECO 
 0036:32  T+4:31 Stage 1 sep 
 0036:38  T+4:37 Stage 2 burn 324s  
 0036:48  T+4:47 Fairing sep 
 0042:02  T+10:01 SECO 1  165 x 212 x 29.2 
 0053:01  T+21:00 Stage 2 restart 37s 
 0053:38  T+21:37 SECO 2  340? x 1140? x 28.6 
 0139:29  T+1:07:28 Stage 2 restart 41s 
 0140:10  T+1:08:09 SECO 3  1085? x 1372? x 28.6  
 0141:53  T+1:09:52 Stage 2 sep  
 0142:30  T+1:10:29 Stage 3 burn 
 0143:57  T+1:11:56 TECO 
 0145:50  T+1:13:49 PAM-D sep 
 0145:52  Yo-yo deploy 
 0202:00  Stage 2 depletion 25s  764 x 1296 x 26.9  
 0202:15  Stage 2 tumble 
1998 Jan 10    655.23 1186 x 36036 x 23.7 
1998 Jan 12  0225? AKM burn 
1998 Jan 13    1442.75 35690 x 36143 x 4.2 GEO 43.2W+1.6W 
1998 Jan 24    1426.77 35560 x 35647 x 4.2 GEO 24.0W+2.3E 
1998 Mar 5    1435.96 35753 x 35814 x 4.2 GEO 6.0E 
1998 Apr 21    1436.07 35771 x 35800 x 4.0 GEO 6.0E 
1998 Apr   Move out 
1998 May 5    1430.85 35545 x 35822 x 4.0 GEO 28.7E+1.3E 
1998 May 20   Transfer to MoD 
1998 Jul 11  Move in 1436.07 35783 x 35788 x 3.9 GEO 53.0E 
1999 Jul 28    1436.05 35782 x 35788 x 3.3 GEO 52.9E 
1999 Aug 6   move out  
1999 Oct 15    1439.78 35781 x 35935 x 3.1 GEO 34.4W+0.9W 
1999 Nov 18    1436.12 35779 x 35794 x 3.1 GEO 33.9W 
2000 Oct 4    1436.11 35783 x 35789 x 2.5 GEO 34.0W 
2002 Oct 26    1436.11 35780 x 35792 x 1.4 GEO 33.9W 
2002 Nov 21    1430.52 35559 x 35795 x 1.4  
2003 Jan 31   mv in  1436.20 35777 x 35796 x 1.3 GEO 38.9E 
2003 Dec 2    1436.02 35779 x 35791 x 1.4 GEO 39.1E 
2003 Dec   Move out of GEO 
2004 Mar   mv in  1436.16 35775 x 35800 x 1.5 GEO 34.1W 
2004 Aug 11    1436.09 35774 x 35799 x 1.7 GEO 34.1W 
2006 Jul 30    1436.18 35781 x 35795 x 3.1 GEO 34.4W 

UARS

 1991-063B


The Upper Atmosphere Research Satellite, built by General Electric, used the Fairchild MMS bus (like Landsat D). It had a total mass of 6526 kg at deployment per the SODB; 6540 kg per the press kit. The satellite was launched on STS-48. The RMS grappled the satellite at 2300 on Sep 14, and it was finally deployed at 0423:02 on Sep 15 into a 563 x 574 km x 57.0 deg orbit. Orbit raising burns were made at 1035 on Sep 17 and 1036 on Sep 18.


UARS 
 

DateTimeEventOrbit  

1991 Sep 14  2300  RMS grapple UARS 
1991 Sep 15  0423:02 RMS deploy UARS   
1991 Sep 15   563 x 574 x 57.0 
1991 Sep 17    563 x 574 x 57.0 
1991 Sep 17 1035 orbit raise  555 x 587 x 57.0 
1991 Sep 18 1036  orbit raise 574 x 575 x 57.0 
1991 Sep 24 0230  574 x 581 x 57.0 
1991 Sep 30 1200  574 x 581 x 57.0 
1992 Jul   ISAMS failed 
1993 May   CLAES cryogen depleted 
1999?   End of orbit maintenance 
2005 Sep 17    550 x 560 x 57.0 
2005 Sep 22?   Begin perigee lower 
2005 Oct 5   Burn  507 x 558 x 57.0 
2005 Oct 6   Burn  473 x 556 x 57.0 
2005 Oct 12   Burn  442 x 555 x 57.0 
2005 Oct 18   Burn  415 x 554 x 57.0 
2005 Dec 8   Burn  
2005 Dec 14  1716  decommissioned 
2011 Sep 24  0400  Entry over Pacific 14.1S 170.2W 

Payload:

  • MMS HPM MMS Hydrazine Propulsion Module, 4 x 5lb thrusters

  • MMS MACS MMS Modular Attitude Control System. This unit originally flew on Solar Max, and was returned to Earth by Shuttle Mission 41-C in 1984 for refurbishment.

  • SUSIM 2 Solar UV spectral irradiance monitor; 1000-4000A solar spectrum. 2 spectrometers in one instrument.

  • CLAES Cryogenic Limb Array Etalon Spectrometer

  • ISAMS Improved Stratospheric and mesospheric sounder

  • MLS Microwave Limb Sounder, 1.6m reflector, 63, 183 and 205 GHz

May 13,2026

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