Thursday, May 28, 2009

The pocket idiot's guide to wedding etiquette

 https://welib.org/md5/1b4d62a88a1a34084610a2db510421f7

Superbird A

 1992-084A


Space Communications Corp.'s Superbird A satellite was the main payload on an Ariane 4 launch. Mitsubishi played prime/integration role on this particular satellite.

The 1155 kg satellite carried 510 kg stationkeeping fuel and 1115 kg orbit insertion fuel for a launch mass of 2780 kg. Solar panel span was 20.3m.

Superbird A was stationed over the Pacific at 158E.


Superbird A
 

DateTimeEventOrbit  

1992 Dec 1  2248  Launch by Ariane 42P (V55)  CSG ELA2 
 2249  PAP sep (T+1:30) 
 2251  Stage 1 sep (T+3:28) 
 2251  Stage 2 MES (T+3:30) 
 2252  Fairing sep (T+4:23) 
 2253  Stage 2 sep (T+5:38) 
 2253  Stage 3 MES (T+5:43) 
 2306  Stage 3 MECO (T+18:11) 
 2308  Superbird sep from H10+ (20:42) 
 2308  Stage 3 sep (T+20:46) 
 2310  Stage 3 end of mission (T+22:23) 
1992 Dec 2  0100? Solar array deploy 
   635.83 237 x 35994 x 7.2 
1992 Dec 3  0100? AKM 1 
   818.43 9428 x 35781 x 2.7 
1992 Dec 5  s  AKM 2 
1992 Dec 7  s  AKM 3 
1992 Dec 10    1436.57 35751 x 35840 x 0.1 GEO 156.7E+0.1W 
1992 Dec 12    1436.09 35758 x 35814 x 0.1 GEO 158.1E 
1993 Jan 15    1436.12 35773 x 35800 x 0.1 GEO 158.0E 
1993 Feb 16    1436.11 35772 x 35801 x 0.0 GEO 158.0E 
1994 Sep 22    1436.11 35775 x 35797 x 0.0 GEO 158.0E 
1996 Sep 19    1436.11 35767 x 35806 x 0.0 GEO 158.1E 
1999 Oct 18    1436.09 35775 x 35797 x 0.1 GEO 158.1E 
2006 Aug 2    1436.09 35762 x 35810 x 0.8 GEO 158.0E 
2008 Dec 21    1436.11 35766 x 35807 x 3.1 GEO 158.0E 

Echostar 5

 1999-050A


Echostar V is an FS-1300 satellite, and will supplement the Echostar DISH network. Launch by AC155 (Atlas 2AS) to 43705 km apogee. Its geostationary station was at 110W. Launch weight was 3177 kg. In 2006, the satellite was moved to 129W and leased as a provider for Ciel Satellite Comms of Canada, the first satellite in a partnership with SES Americom. It was renamed Ciel 1.


Echostar 5 
 

DateTimeEventOrbit  

1999 Sep 23  0602 Launch by Atlas 2AS (AC-155) CC LC36A 
  T+0:53 SRM 1-2 burnout 
  T+0:57 SRM 3-4 burn 
  T+1:15 SRM 1-2 sep 
  T+1:52 SRM 3-4 burnout 
  T+1:55 SRM 3-4 sep 
  T+2:43 BECO 
  T+2;46 Booster sep 
  T+3:21 Fairing 
  T+4:57 SECO 
  T+4:59 Atlas sep 
  T+5:16 MES1 
 0611 T+9:51 MECO1  90.98 156 x 475 x 28.2 
 0626 T+24:42 MES2 
 0628 T+26:20 MECO2  166 x 45822 x 26.55 
 0630 T+28:56 Centaur sep 
1999 Sep 24    827.93 131 x 45526 x 26.6 
1999 Sep 25?   LAM-1 
1999 Sep 28?   LAM-2 
1999 Sep 28    972.71 21848 x 30434 x 0.8 
1999 Sep 30?   LAM-3 
1999 Oct 3?  LAM-4 
1999 Oct 3    1403.05 34506 x 35767 x 0.4 GEO 112.9W+8.5E 
1999 Oct 6    1435.82 35752 x 35809 x 0.2 GEO 109.7W 
1999 Oct 12    1436.09 35773 x 35799 x 0.2 GEO 110.0W 
1999 Nov 5    1436.09 35775 x 35797 x 0.1 GEO 110.0W 
2003 Mar 1    1436.09 35778 x 35794 x 0.1 GEO 110.2W 
2003 Mar 5   Leave 110W 
2003 Mar 22   Arrive 119W 
2003 May 9    1436.08 35772 x 35799 x 0.04 GEO 119.0W 
2005 Jul 5    1436.07 35772 x 35799 x 0.02 GEO 119.0W 
2005 Jul 6?  Move out of GEO 
2005 Jul 22   Arrive 129W, Ciel operations 
2006 Apr 3    1536.10 35772 x 35800 x 0.05 GEO 128.9W 
2006 Aug 4    1436.09 35776 x 35796 x 0.0 GEO 128.9W 
2009 Mar 19  1436.09 35773 x 35799 x 0.2 GEO 148.0W 

Wednesday, May 27, 2009

STS-96 (Discovery)

 1999-030A


STS-96 carried LP (Launch Package) 2A-1. consisting of the Spacehab Logistics Double Module, the Integrated Cargo Carrier, and associated equipment.

Launch mass was 118857 kg; landing mass planned was 100234 kg.

Like STS-88, approach on +R-bar, then fly around and above to do final approach on -R-bar, since without the SM the FGB antennas must be nadir pointing to allow commanding from ground stations.

With Tammy Jernigan on the RMS and Dan Barry floating, Julie Payette as IV and Ellen Ochoa as RMS operator, one EVA was planned.

Install foot stanchion on RMS, Jernigan on RMS. The US and Strela cranes would be installed, then foot restraints which work for both US and Russian EVA boots were added added to PMA-1 and Unity. Barry adds a mask to the docking target. Next, the SHOSS bags were transferred. A final task was to add a thermal cover to the Unity trunnion pin.

The astronauts transferred 311 kg of water and 1307 kg of cargo to ISS. 89 kg of ISS equipment was returned to Discovery,and 300 kg of equipment was installed during the EVA.


STS-96 
 

DateTimeEventOrbit  

1999 Apr 15  1600  Roll from OPF/1 to VAB/3 
1999 Apr 16   Mate to ET 
1999 Apr 23   Roll to LC39B 
1999 May 16  0735  Rollback to VAB1 
1999 May 27  1049:42  Launch  LC39B 
 1051:46  T+2:04 SRB sep 
 1051:57  OMS Assist 1:42 
 1053:39  OMS assist C/O 
 1058:04 T+8:21 MECO  88.32 74 x 308 x 51.6 
 1058:24  ET sep 
 1132:53 T+43:21 OMS-2 2:44 77.8m/s  89.83 187 x 344 x 51.6 
 1135:37  OMS-2 CO 
 1224  PLBD open 
 1349:24 T+3:43 OMS-3 NC1 13m/s  91.19 324 x 341 x 51.5  
 1349:52  RCS trim 0.5s 
 1435:53  OMS-4 NC2 19s 10m/s 
1999 May 28  0302:53  RCS NC2 19s 1.5m/s 

0714?  RMS uncradle for survey 
 0855 RMS reberth 
 1918:54  RCS NC3 14s 1m/s 
 2349:31  RCS NC4 19s 1.5m/s 
1999 May 29  0037:35  RCS NCC 4s 0.5m/s 
 0135:17  OMS-5 L TI burn 10s 2.3m/s 
 0155:17  RCS MC1 0.2m/s 
 0228:17  MC2 0.3m/s 
 0245:17  MC3 
 0255:17  MC4 
 0305s 0:00 Arrive +R-bar 
  0:16 TORRA flyaround 
  0:28 +V-bar crossing 
 0332s 0:39 -R-bar arrive 100m 
  Approach 
 0337s Pause at 50m 
 0413s Pause at 10m 
 0424  T+1:18:29 Dock ISS PMA-2 
 0437:37  Hard dock 
 0700?  PMA-2 Hatch open 
1999 May 30  0034  RMS checkout 
  Depress EAL 

0256  EVA begins (battery) Jernigan, Barry 
 0258:24 AL depress (MR) 
  HO 
 0325  Tether drifts loose 
 0411s OTD install 
 0511s  Strela install 
 0611s  Tool bags install 
  HC 
 1051:32  EVA ends (repress) 7:55 
1999 May 31  0114  HO to Unity 
 0207  HO to Zarya 
  Comm system repair 
  Battery repair 
1999 Jun 1  Noise insulation in Zarya 
  Supply transfers 
1999 Jun 3  0640  HC to Zarya 
 0712  HC to Unity 
 0844  HC to PMA-2 (79:30) 
 0936:53  RCS reboost, 37min 

2239:17  Undock(5:18:17) 
  At 140m on -R-bar 
 2257s Begin flyaround 
 2343s On -Rbar, begin 2nd flyaround 
1999 Jun 4  0006  Cross +Rbar on Flyaround 2 
 0030  On -Rbar, begin 3rd flyaround 

0053:19 Sep burn at +R-bar 12s 1m/s 
 0106 Recross +R-bar at 600m 
 2348s RCS hot fire test 
1999 Jun 5  0721  Starshine eject 
1999 Jun 6  0214:20  PLBD close 
 0454:09  Deorbit 3:39 114m/s 
 0457:48  OMS-6 DO CO  
 0530:49  Entry interface 
 0602:45  Landing KSC RW15 
 0602:50Drag chute 
 0602:57NGTD 
 0603:39  WS 

Sunday, May 24, 2009

Panamsat 6B

 1998-075A


PAS 6B is an HS-601HP satellite for an AOR satellite providing Sky's DTH transmissions for S America from 43W. Launch by Ariane in 1998. It supplemented PAS 6, a Loral satellite which had problems with solar arrays. Mass is 3594 kg launch, 2134 kg BOL. Size is 3.4 x 2.8 x 6.0m with 26.2m span. PAS 6B developed trouble with its XIPS engine in June 2003.


PAS 6B 
 

DateTimeEventOrbit  

1998 Dec 22  0108  Launch by Ariane 42L 
  T+2:22 PAL sep 
  T+3:14 Stage 1 sep 
  T+4:07 Fairing sep 
  T+5:27 Stage 2 sep 
  T+5:32 Stage 3 burn 
 0126 T+18:43 Stage 3 MECO 
 0128 T+20:40 Sep from H-10  228 x 35717 x 7.0 
1998 Dec 22    630.28 221 x 35724 x 7.0 
1998 Dec 24  0046? LAM-1 
1998 Dec 24    634.16 424 x 35720 x 7.0 
1998 Dec 25  1900? LAM-2 
1998 Dec 26    781.59 7689 x 35768 x 3.3 
1998 Dec 29  0100? LAM-3 
1998 Dec 30    1197.66 26182 x 35777 x 0.6 
1998 Dec 30  1650? LAM-4 
1998 Dec 30    1365.49 32995 x 35790 x 0.2 
1999 Dec 31?  LAM-4 
1999 Jan 1?  LAM-5 
1999 Jan 3    1436.44 35783 x 35802 x 0.1 GEO 46.5W+0.1W 
1999 Feb 2    1436.07 35777 x 35794 x 0.0 GEO 46.0W 
1999 Feb   mv out 
1999 Mar 10    1436.15 35780 x 35794 x 0.0 GEO 43.1W 
1999 Nov 7    1436.16 35782 x 35793 x 0.1 GEO 43.2W 
2002 Jul 11    1436.07 35781 x 35790 x 0.0 GEO 43.2W 
2003 Jul 3    1436.14 35776 x 35798 x 0.1 GEO 43.3W 
2006 Aug 1    1436.11 35776 x 35796 x 0.0 GEO 43.1W 
2008 Mar 1    1436.15 35777 x 35797 x 0.0 GEO 43.1W

May 13,2026

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