Saturday, December 19, 2009

STS-103 (Discovery)

 1999-069A


Launch mass is 113881.9 (112563 in retrospective data). Sep mass of ET is 109965.3 kg. 3 EMUs carried. TCS. One HST-PFR in 13P and one on the FSS.

EVAs were carried out through the axial (longitudinal) hatch on the EAL. On the first EVA, the astronauts replaced HST's 6 gyros, the crucial mission task. Next, they fought with the valve covers on the NICMOS vents; they had planned to open the valves by hand and with a power ratchet tool, but in the end they had to go and get a pistol grip tool to remove the covers. The vents open, any remaining N2 will be vented by the time the new neon cooling system is installed on SM-3B. One of the old gyros wouldn't fit properly in the COPE at first, but eventually the crew managed to shove it in. The third task on EVA 1 was installation of Voltage Improvement Kits intended to prolong the life of the spacecraft's batteries. The walk was extended to allow the crew to install all six kits.

EVA-2 saw the installation of an Intel-486 based computer in the spacecraft.

During prep for EVA-3, Grunsfeld's suit had a problem, so he wore Foale's suit instead. On EVA-3, two bays were covered with the new outer blanket layers. There wasn't time to cover four more bays, so that was left for SM-3B.

 


STS-103 
 

DateTimeEventOrbit  

1999 Nov 4  1500  Roll from OPF/1 to VAB/1 
1999 Nov 5   Mate to ET in VAB/1 
1999 Nov 13  1227  Roll to LC39B 
1999 Dec 16   Scrub at T-11h 
1999 Dec 17   Scrub 
1999 Dec 20  0050:00  Launch  KSC LC39B 
 0052:04  SRB sep 
 0058:26  MECO  90.89 56 x 587 x 28.5 
 0058:45  ET-101 sep 
 0134:08  T+44:00 OMS-2 2:33 75.2m/s  313 x 579 x 28.5 
 0136:41  OMS 2 CO 
 0149   93.63 320 x 583 x 28.5 
 0230 PLBD open 
 0615:30 OMS-3 NC-1 91s 46m/s 
 0617:02 OMS-3 CO 
 1400   95.32 484 x 583 x 28.5 
 1930s RMS tests 
1999 Dec 21  0431:20 OMS-4 NSR 47s 24m/s 
 0432:08  OMS-4 CO 
 0432:23  RCS NC-1 trim  0.4s 
 0526:49 RCS NC-2 31s 2m/s 
 0527   96.28 570 x 589 x 28.5 
 1826:22  OMS-5 R NC-3 20s 5m/s 
 1826:42  OMS-5 CO 
 1826:55 NSR trim 0.2s 
 1914:34 OMS-6 L NH 17s 4m/s 
 1914:51  OMS-6 CO 
 2128:00 RCS NCC 1s 
 2228:06 TI 9s, 1.3m/s, mass 104144 kg 
 2248:06  MC-1 2s 
 2322:58 MC-2 5s 
 2339:58 MC-3 2s 
 2349:58 MC-4 7s 
1999 Dec 22  0002  On -Rbar at 207m 

0034:01  Grapple 591 x 610 x 28.5 
 0133  Berth on FSS 
 0142:00 Latched 
 0203  On external power 
 0208  RMS ungrapple 
 0600   96.71 591 x 610 x 28.5 
 1838  Depress at 1psi 
 1841:37  EVA depress end 
 1852? HO (TC closed), axial hatch 

1854  EVA-1 on battery (Smith, Grunsfeld) 
 1901  Thermal cover open 
 1902  Egress EV1 
  Grunsfeld on RMS 
 2018  Prep to change RSU2 
 2050? RSU-2R out of ORUC 
 2119  RSU-2 removed 
 2130? RSU-2R installed 
 2135? RSU-2 in ORUC 
 2135  RSU-3R out of ORUC 
 2156  RSU-3 removed 
 2210? RSU-3R installed 
 2215?  RSU-3 in ORUC 
 2215?  RSU-1R out of ORUC 
 2235  RSU-1 removed 
 2243  RSU-1R installed 
 2250? RSU-1 in ORUC 
  Difficulty closing RSU-1 in box 
 2250  Attempt to open NICMOS valves 
 2333  Second attempt 
1999 Dec 23    
 0006  NICMOS cooling valves opened 
 0108  Begin Voltage Improvement Kit work 
 0129  VIK 1-3 into Bay 3 
 0150  Begin VIK 4-6 into Bay 2  
 0208  VIK install complete 

0252  Ingress 
 0258  Thermal cover closed 
 0302  Hatch closed 
 0306  Repress begins  
 0309:28 Begin repress (STS MR) 

0310  EVA-1 off battery, 8:15 
 0310  Repress, NASA dur 8:15:10, JCM dur 8:32 
  EVA-2 Foale, Nicollier  
 1828  Depress begins 
 1845  Airlock at 2psi : DEPRESS? 
 1852:33 Depress complete (MR) 
 1855  Depressurized at 0.2psi 
 1900  Hatch open 
 1905:56 EVA-2 on battery 
 1913  Thermal cover open, egress 
 1938 Foale on RMS 
 2015  DF-224 computer removed 
 2045?  DF-224 stowed 
 2050? HST-486 out of ORUC 
 2120 HST-486 computer installed 
 2200?  Foale off RMS, Nicollier on RMS 
 2341  FGS-2R removed from HST 
 2357  FGS-2 out of ORUC 
1999 Dec 24  0043 FGS-2 installed in HST 
 0140?  FGS-2R stowed in ORUC 
 0303  Ingress; dur 7:50  
 0307  HC; dur 8:07 
 0311  Begin repress, on orbiter power 
 0316:19  Repress : NASA dur 8:10 JCM depress dur 8:31  
  EVA-3 Grunsfeld, Smith 
 1848  Go for depress 
 1909:51 Depressurized (MR) 
 1915? Inner hatch open  
 1917  Depress complete 
 1917  On battery EVA-3 
 1926  Thermal cover open 
 1927  Egress 
  Grunsfeld on RMS 
 2200   96.71 590 x 610 x 28.5 
  NOBL layers added 
1999 Dec 25  0202  Off RMS 
  Rotate telescope 
 0255  Ingress 
 0301 Thermal cover closed 
 0307 Hatch closed 
 0318 Grunsfeld EMU failed to switch to OV power 
 0325:48 Repress 8:08 NASA; JCM 8:15 

 
 2000:30  RMS grapple HST 
 2118:41  HST unberth 
 2303:01 Release T+6:21:28 
 2303:45 Sep-1 RCS 5s 0.4m/s 
 2338:54 Sep-2 RCS 5s 0.4m/s 
1999 Dec 26  2108:30  RCS adjust 95s 7m/s lower peri 28km 
1999 Dec 27  0600   96.40 562 x 609 x 28.5 

1827  PLBD closed 
 2248:26 Deorbit 4:49 157m/s  50 x 616 x 28.4 
 2253:15  OMS DO CO 
 2329:41  Entry Interface 
1999 Dec 28 0000:47 MGTD KSC RW33 7:23:10:47 
 0000:58 NGTD 
 0001:34 WS 

Friday, December 18, 2009

Terra

 1999-068A


Terra (EOS AM-1) was the first large EOS satellite. Earth Observing System AM-1 is built by LMT (formerly Astro Space) Valley Forge. Terra is the first NPOESS satellite. Launch of the spacecraft into 705 km 98.2 deg 10:30am SSO is by ILS Atlas 2AS AC-141 from V SLC3E in 1998 Dec. The stretched 14' EPF fairing was used for the first time. Launch mass 4854 kg full, with 328 kg hydrazine.Total 4765 kg at separation.

Control will be from the GSFC EOS Control Center. Launch was delayed due to problems with the ground ops software. 6.8m long 3.5m dia. box + 10m solar array. Box + 1 panel; bus has heritage from UARS.

The plan was to fly Terra in the same orbit as Landsat 7, but that was delayed when the first orbit raise burn was aborted due to a roll problem.


Terra 
 

DateTimeEventOrbit  

1999 Dec 18  1857:39  Launch by Atlas IIAS  V SLC3E 
  T+00:59 SRB 3-4 burn 
  T+1:44 SRB1-2 sep 
  T+1:58 SRB3-4 sep 
  T+2:46 BECO 
  T+2:49 Booster sep 
  T+3:11 Fairing 
  T+4:42 Atlas MECO 
  T+4:44 Atlas sep 
 1902:40 T+5:01 Centaur MES 
 1908:49 T+11:10 Centaur MECO  98.01 653 x 673 x 98.3  
 1911:19  T+13:40 Centaur sep  98.26 655 x 695 x 98.3 
 1925Centaur depletion  355 x 654 x 98.3 
1999 Dec 18    98.14 654 x 684 x 98.2 
2000 Jan 11   AOCS-1 burn
2000 Jan 31    98.16 655 x 686 x 98.2 
2000 Feb 17    98.48 684 x 687 x 98.2 
2000 Feb 23   Final AOCS-8 burn
2000 Mar 30    98.83 701 x 703 x 98.2 
2000 May 25    98.83 699 x 705 x 98.2 
2002 Aug 4    98.82 701 x 703 x 98.20 
2003 Jul 6    98.82 701 x 703 x 98.18 
2005 Oct 21   small collision avoidance burn 
2007 Jun 22   COLA to avoid FY1C deb, 1.3 km raise 

Payload:

  • CERES Clouds and the Earth's Radiant Energy System

  • MODIS-N Moderate Res Imaging Spectrometer

  • MISR Multi Angle Imaging Spectroradiometer

  • ASTER Adv Spaceborne Thermal Emision and Reflection Radiometer

Monday, December 14, 2009

Sirius 5

 2000-077A


The third Sirius CD Radio satellite was launched on 2000 Nov 30.


Sirius 3 
 

DateTimeEventOrbit  

2000 Nov 30  1959:47  Launch by Proton-K/DM3 17L KB LC81/23 
  T+2:00 St 2 MES 
  T+2:06 St 1 sep 
  T+5:30 St 2 MECO 
  T+5:32 St 3 sep 
  T+5:35 St 3 MES 
  T+5:44 Fairing sep
 2009 T+9:30 St 3 MECO 
 2009:37 T+9:49 St 3 sep 
 2009 Adapter sep 
 2043:27 T+43:40 DM MES-1 375s 
 2049:42 T+49:55 DM MECO-1  200? x 24400? x 63.4 
 2203:04 T+2:03:17 DM MES-2 113s 
 2205 T+2:05:10 DM MECO-2 
 2225 T+2:25:10 DM sep 
2000 Dec 2    994.81 6177 x 47087 x 63.4 
2000 Dec 4   LAM-1 1142.07 12539 x 47089 x 63.4 
2000 Dec 6  1100? LAM-2 1417.13 23749 x 47049 x 63.4 
2000 Dec 13    1435.89 24491 x 47073 x 63.4  
2000 Dec 20    1435.89 24486 x 47078 x 63.4 GSO 66.0W 
2006 Aug 2    1435.96 24363 x 47204 x 63.6 GSO 64.9W

May 13,2026

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