Friday, October 21, 2011

Turksat 1C

 1996-040B


Turksat 1C was lauched by Ariane for Aerospatiale, which delivered it on orbit to Turk Telecom. Launch mass was 1743 kg, BOL mass 1078 kg and dry mass 789 kg. The satellite is 1.64 x 1.46 m x 2.20 m with a 22.20 m span. It was built by Aerospatiale-Cannes. The satellite was launched in the lower Ariane position, underneath the SMS (Stretched Mini Spelda) structure. It provides services to Turkey. Initial test position is 31.3E, then service position is 42E.


Turksat 1C 
 

DateTimeEventOrbit  

1996 Jul 9  2224  Launch by Ariane 44L (V88)  CSG ELA2 
 2227  Stage 1 sep T+3:32 
 2229  Stage 2 sep T+5:43 
 2229 Stage 3 TIG T+5:48 
 2242  Stage 3 MECO T+18:45 
 2244  Arabsat 2A sep T+20:00 
 2246  SMS sep T+22:52 
 2248  Turksat sep T+24:20 
1996 Jul 11    630.00 212 x 35718 x 7.0 
1996 Jul 11  1130? LAM-1 
1996 Jul 11    755.49 6476 x 35722 x 3.4 
1996 Jul 12  1230? LAM-2 
1996 Jul 12    1299.66 30345 x 35798 x 0.2 
1996 Jul 14  0730? LAM-3 
1996 Jul 14    1434.18 35688 x 35810 x 0.1 GEO 29.9E+0.5E 
1996 Jul 20    1435.81 35775 x35786 x 0.1 GEO 31.4E 
1996 Jul 22    GEO 31.3E+0.1/d 
1996 Aug 6    1436.02 35773 x 35796 x 0.1 GEO 31.3E 
1996 Sep 14    1436.00 35769 x 35799 x 0.0 GEO 31.5E 
1996 Sep   Move to 42E 
1996 Oct 4    1436.07 35773 x 35799 x 0.0 GEO 42.0E 
1999 Oct 15    1436.09 35777 x 35795 x 0.0 GEO 42.0E 
2006 Aug 1    1436.06 35768 x 35803 x 0.1 GEO 42.0E 
2008 Jul 30   GEO 42E, move to 30E 
2008 Aug 24    1436.03 35772 x 35798 x 0.4 GEO 31.0E 
2010 Jan 29    1436.08 35771 x 35800 x 2.2 GEO 31.0E 

December 29,1998

 https://web.archive.org/web/20080504033425/http://digest-archive.degrassi.ca/DD53.htm

Monday, October 17, 2011

ST-5

 2006-008A


Each Nanosat Constellation Trailblazer is 25 kg, 0.52m dia 0.48 high oct prism with an extendable boom for 1.0m? span. Three satellites on a single launch to 300 x 4500 km x 97 deg on Pegasus XL from Vandenberg. Built by GSFC. Will study magnetosphere; spacecraft highly magnetically clean to allow short mag booms.


ST5 
 

DateTimeEventOrbit  

2006 Mar 14  1327 L1011 T/O V RW30/12 
 1428  Abort  
 1448s  Land on RW12  
2006 Mar 22  1304  L1011 T/O V RW30/12 
 1403:45 Drop  
 1403:50 T+0:05 Stage 1 on 70s 
 1405:02 T+1:17 Stage 1 burnout 
  Stage 1 sep 
 1405:16 T+1:31 Stage 2 on  
 1405:55 T+2:10 Fairing sep, 115 km  
 1406:29 T+2:44 St 2 burnout, 156 km 
 1409:02 T+5:17 Stage 2 sep 
 1409:02 T+5:17 Stage 3 burn 283 km  
 1410:09? T+6:24? Stage 3 burnout 
 1413:16s T+9:31 ST5-FWD sep S+0 
 1416:26 T+12:41 ST5-2 sep S+200s 
 1419:36 T+15:51 ST5-3 sep S+390s  301 x 4568 x 105.6  
  Pegasus CCAM  
 1532   298 x 4554 x 105.6  
2008 Jun 30   end of ops

Payload:

  • X-band transponder, Aero Astro comms system

  • CULPRIT Low power microelectronic device, CMOS ultra low power radiation tolerant logic.

  • Cold gas microthruster, Fine attitude adjustment

  • Lithium ion power system

  • Magnetometer booms, 0.36m long

May 13,2026

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