Monday, June 20, 2005

Aviation Week: November 22,2004

 https://welib.org/md5/5d6ba8419de8f0f15379ecfff08d23f3

ADEOS-2

 2002-056A


ADEOS 2 has a mass of 3680 kg. Size 6 x 4 x 4m, 28 m span, Irreg + 1 panel. GLI will have 36 bands, 1 km res. AMSR has 10 km res at high freq. This was the first launch since MHI took over launch operations from NASDA on Nov 20. Communications with the satellite failed in Oct 2003, almost exactly the same interval after launch as the ADEOS-1 failure.


ADEOS-2 
 

DateTimeEventOrbit  

2002 Dec 14  0131  Launch by H-2A 
  T+1:40 SRB-A burnout 
  T+1:47 SRB-A sep 
  T+4:20 5S PLF sep 
  T+6:35 St 1 MECO 
  T+6:43 St 1 sep 
 0137 T+6:49 St 2 MES  -5600? x 500?  
 0146 T+15:38 St 2 MECO 
 0147 T+16:28 ADEOS sep  804 x 806 x 98.7  
 0201 T+30:55 Fedsat sep 
 0203 T+32:40 WEOS sep 
 0205 T+34:30 MuLabSat sep 
2002 Dec 17   Intersat comms antenna deploy 
2003 Oct 24   In safemode 
 2300  Power and comms unstable, LOS 

Payload:

  • AMSR Adv Microwave scanning radiometer 6.9-53 GHz

  • GLI Global Imager; Ocean, land and cloud, 3750A-12.5mu

  • IOCS Inter-orbit comms system

  • SeaWinds Wind speed sensor.

  • CCR Corner cube reflector

  • DCS Data collection system

  • POLDER Polarization and Directionality of Earth Reflectance

  • VMS ODV-4 visual monitoring system (TV camera to observe solar paddle)

STS-100 (Endeavour)

 2001-016A


STS-100 carried out mission 6A, delivering the SSRMS arm Canadarm-2. Press kit quotes Launch mass was 103504 kg; landing mass was to be 99740 kg. However, mass post NC2 burn was almost 114000 kg. Deorbit mass was around 99000 kg.

The mission was extended two days when ISS computer failures delayed the end of SSRMS tests.


STS-100 
 

DateTimeEventOrbit  

2001 Mar 17  Tow from OPF/2 to VAB/3 
2001 Mar 19  Mate with ET 
2001 Mar 22   Roll to LC39A 
2001 Apr 19  1840:42  Launch 
 1842:46  SRB sep 
 1842:56  OMS-1 assist 
 1844:38  OMS-1 CO 
 1849:08  MECO 
 1849:27  ET sep  74 x 329 x 51.6 
 1924:24  OMS-2 54s 25m/s  89.39 159 x 329 x 51.6 
 1925:18  OMS-2 CO 
 2017:07  PLBD open 
 2223:19  OMS-3 NC1 burn 26m/s 90.23 242 x 328 x 51.6  
 2224:11  OMS-3 CO 
2001 Apr 20  1042:37  OMS-4 R NC2 burn  90.31 247 x 332 x 51.6  
 1042:48  OMS-4 CO 
 2052:12  OMS-5 NC3 burn 36m/s  91.61 331 x 375 x 51.6 
 2053:30  OMS-5 CO 
2001 Apr 21  0900  0.1m/s burn 

0944:53 OMS-6 NC4 burn 13.4m/s  
 0945:21  OMS-6 CO 
 1117:25  OMS-7 L TI burn 2.8m/s 
 1117:38  OMS-7 CO 
 1137:24  MC1 0.5m/s 
 1214:18  MC2 0.6m/s 
 1231:18  MC3 0.2m/s 
 1241:18  MC4 0.1m/s 
 1256  On -Rbar at 200m 
 1310  On Vbar at 94m 
 1324  Approaching at 70m 
 1328  At 57m 
 1338  At 36m 
 1341  At 30m 
 1347  At 20m 
 1353  10m on final approach 
 1358:49  Docking at PMA-2 
 1410:42  Hard dock  92.22 375 x 391 x 51.6 
2001 Apr 22    
 0810  RMS uncradle 
 0823:41 RMS grapple SLP 
 0842  SLP unberthed 
 1042  SLP berthed to LCA 
 1117:58 RMS ungrapple SLP 
  EVA-1 Hadfield, Parazynski 
 1131  Begin depress 9psi 
 1134  At 5psi 
 1138  Resume depress 
 1143:02  Depress complete 
 1144? HO 
 1145  Battery power 
 1152  TC open 
 1152  Egress EV1 
 1158  Egress EV2 
 1302  UHF ant unberthed from SLP by Hadfield on RMS 
 1330  UHF antenna install complete 
 1500  SSRMS boom raised 
  SSRMS bolts fastened 
 1810? Ingress EV2 
 1835  Ingress EV1 
 1839  TC closed 
 1845  HC  
 1855:27  Repress 7:10:12 (NASA) 
 2005  RMS recradle 
2001 Apr 23  0930  HO to ISS 
 1114  SSRMS LEE-B unberthed from SLP 
 1416  SSRMS LEE-B grapple Destiny PDGF 
 1425:57  MPLM grappled by RMS 
 1458  MPLM unberthed from bay 
 1458  RMS lifting MPLM 
 1600  Raffaello berthed to Unity -Z 
 1616:03  MPLM ungrapple 
 1926  HC to ISS 
 1950:54  Reboost-1 59:36 2.3m/s 
2001 Apr 24   EVA-2  
 1222  Begin depress 
 1231:29 Depress 
 1232? HO 
 1234  Battery power 
  TC open 
 1240? Egress 
 1455  SSRMS power connected 
 1428  Early COMM antenna removed from Unity 
 1825  SLP unberth from LCA, on SSRMS LEE-A 
 1905  DCSU unberth 
 1916  DCSU berthed to Destiny ESP 
 1950  EV1 Ingress 
 2000  EV2 ingress 
 2001? TC closed 
 2003  Hatch closed 
 2013:18  Repress 
 2130? Hatch open to ISS 
2001 Apr 25   Computer problems on ISS 
2001 Apr 27  1120:42  Reboost-2 60:00 4.8m/s 
 1806:38 RMS grapple MPLM 
 2003  MPLM unberthed from Unity 
 2059  MPLM berthed in bay 
 2105:39  RMS ungrapple MPLM 
2001 Apr 28  2043:42  RMS grapple SLP 
 2056  SSRMS latches release SLP 
 2102  SSRMS ungrapple SLP 
 2251  RMS berth SLP 
 2257:27  RMS ungrapple SLP 
2001 Apr 29  1620  Hatches closed to ISS 
 1734:04  Undocking along +Vbar 1m/s 
 1754  Begin flyaround at 100m 
 1801  On +Rbar 
 1815  On -Vbar at 200m 
 1828  Sep burn on +Rbar 
2001 May 1  1058 PLBD closed 
 1502:47  OMS DO 3:34 EAFB186 0.111km/s 
 1506:20  OMS DO cutoff  
 1539:17  Entry interface 
 1610:43 Landed on EAFB RW22 11d:21:30:00 
 1610:53  NGTD 
 1611:56  Wheels stop 
2001 May 8  1330SCA 905 depart EAFB 
 1705SCA arrive at Altus AFB OK 
 1915  SCA depart Altus AFB 
 2022  SCA arrive at Little Rock AFB 
2001 May 9  1533  SCA depart Little Rock AFB 
 1809  SCA 905 landed at SLF RW15 
2001 May 10  0130Tow to OPF/1 

Friday, June 17, 2005

Navstar 37

 1993-032A


Navstar 37 (USA 91) was launched on 1993 May 13. It was stationed at plane C-4 and given the ID PRN 07.


Navstar 37 
 

DateTimeEventOrbit  

1993 May 13  0007:00 Launch by Delta 7925  CC LC17 
  T+0:56 SRM 1-3,7-9 out  
  T+1:01 SRM 4-6 on 
  T+1:02 SRM 1-3 sep 
  T+1:03 SRM 7-9 sep 
  T+1:57 SRM 4-6 off 
  T+2:02 SRM 4-6 sep 
  T+4:25 MECO 
  T+4:31 VECO  
  T+4:33 Stage 1 sep 
 0011  Stage 2 TIG (T+4:38) 
 0011  Fairing sep (T+4:50) 
 0018?  SECO-1 (T+11:37)  186 x 186? x 34.0? 
 0027?  T+20 SES-2 
 0027?  SECO-2  185 x 732? x 34.0  
  T+20:55 spinup 
 0028 T+21 Delta sep 
 0029 T+22 TES 
 0030 T+23 TECO  355.32 171 x 20308 x 37.7  
 0031 T+24 Stage 3 sep   
 0031 T+24 Yo weight  
 0113? SES-3 
  SECO-3 depletion  96.74 472 x 732 x 21.9  
1993 May 14  2118? Star 37XFP burn  716.92 20048 x 20263 x 55.0  
1993 Jun 12   In service 
1993 Aug 22    717.93 20026 x 20335 x 55.0 
1997 Feb 1   Operating at slot C-4 
2003 Dec 20   decommissioned 

XM-3 (Rhythm)

 2005-008A


Launch of XM-3 as backup by Zenit-3SL in 2005. Satellite is a BSS702. It will replace XM1 at 85W, XM1 will move to 115W colocated with XM2, which will be replaced by XM4 in 2007. Accourding to some sources, XM-3 is nicknamed Rhythm.

Launch mass 4703 kg, BOL mass 2950 kg. Size 3 x 3.3 x 7m, with 40.4m span.


XM3 
 

DateTimeEventOrbit  

2005 Mar 1  0351 Launch by Zenit-3SL   
  T+2:30 St 1 sep 
  T+3:46 PLF sep 
 0359 T+8:31 St 2 sep 176 km  -2009 x 178 x 0 
 0359 T+8:41 DM MES-1 
 0408 T+17:10 MECO-1 207 km  180 x 9452 x 0  
 0438 T+47:09 DM MES-2 
 0441 T+50:18 MECO-2  675.71 2491 x 35767 x 0.1 
 0451 T+1:00:58 DM sep 
2005 Mar 1    675.71 2491 x 35767 x 0.1  
2005 Mar 4    739.73 5749 x 35682 x 0.1  
2005 Mar 5    841.50 5757 x 35760 x 0.5 
2005 Mar 7    991.67 17390 x 35735 x 0.3 
2005 Mar 9    1411.47 34824 x 35781 x 0.1 GEO 92.6W+6.3/d 
2005 Mar 11   1431.13 35595 x 35783 x 0.1 GEO 80.1W+1.2E/d 
2005 Mar 11    1435.44 35758 x 35789 x 0.1 GEO 80.1W+0.1E/d 
2005 Mar 12    1436.25 35781 x 35797 x 0.1 GEO 80.1W+0.05W/d 
2005 Apr 10    1436.18 35784 x 35791 x 0.0 GEO 80.1W+0.03/d 

Thursday, June 16, 2005

Kosmos 743

  1975-053A


There is some question as to whether this vehicle used 11A57 or 11A511U: the NK forum in 2010 said it was actually 11A511U. Unlike most Germes flights, Kosmos-743 made several orbital changes.


Kosmos-743 
 

DateTimeEventOrbit  

1975 Jun 12  1230 Launch by Soyuz-U  Plesetsk 
 1234 Blok-I burn 
 1238 Blok-I sep 
1975 Jun 12    89.63 179 x 332 x 62.8 
1975 Jun 13    89.62 180 x 330 x 62.8 
1975 Jun 14   Raise apogee89.77 180 x 345 x 62.8 
1975 Jun 15    89.76 180 x 345 x 62.8 
1975 Jun 16   Lower orbit 89.14 167 x 296 x 62.8 
1975 Jun 19    89.07 167 x 289 x 62.8 
1975 Jun 20   Raise apogee89.24 167 x 306 x 62.8 
1975 Jun 24    89.14 166 x 298 x 62.8 
  Engine sep 
1975 Jun 25   
 0348? Deorbit 
 0358? PO sep 
 0402? Entry 
 0418? Landed 

Tuesday, June 14, 2005

Gambit-3 32

  1971-070A


KH-8 32 was launched on 1971 Aug 12 by Titan IIIB Agena D from Vandenberg on a 22 day flight. This flight was the first to fly the longer focal length R-5 optical system and marked the transition to the long tank Titan 24B. The vehicle was deorbited over Alaska as part of the VAST 3 experiment to recover a 'payload sensor'.


KH-8 32 
 

DateTimeEventOrbit  

1971 Aug 12  1530  Launch by Titan 3B Agena D  V SLC4W 
 1532  Titan stage 1 sep 
 1535 Titan stage 2 sep 
 1535  Agena burn 
 1540? Agena MECO 
 1630   90.20 137 x 431 x 111.0 
1971 Aug 13  0431   90.10 136 x 422 x 111.0 
1971 Aug 15  2358   89.68 127 x 389 x 111.0 
  Orbit raise 
1971 Aug 16  2224   90.04 129 x 423 x 111.0 
1971 Aug 19  1623   89.87 130 x 405 x 111.0 
  Orbit raise 
1971 Aug 20  2220   90.05 131 x 422 x 111.0 
1971 Aug 23  1017   89.74 131 x 391 x 111.0 
 1946  SRV-1 deorbit opportunity 
 1953  Entry 
 2020?  SRV-1 recovered 
  Orbit raise 
1971 Aug 24  0847   90.06 134 x 420 x 111.0 
1971 Aug 28  2045   89.83 132 x 399 x 111.0 
  Orbit raise 
1971 Aug 29  2042   89.98 134 x 412 x 111.0 
1971 Sep 1  0238   89.76 133 x 391 x 111.0 
1971 Sep 2  2023   89.48 132 x 365 x 111.0 
1971 Sep 3   Reentered after 22d 
 2223?  SRV-2 ejected 
 2230?  Entry 
 2255? SRV-2 recovered 
 2347? VAST 3 controlled reentry in Alaska 

Friday, June 10, 2005

People Almanac 2004

https://welib.org/md5/0c12412b75baaf4a3b9c84cf419981f2

Kosmos 1298

 1981-080A



Kosmos-1298 
 

DateTimeEventOrbit  

1981 Aug 21  1020  Launch by Soyuz  KB  
 1028  Blok-I sep 
1981 Aug 21    89.55 174x331x64.9 
1981 Aug 26    89.18 166x303x64.9 from 88.96 162x284 
1981 Aug 30    90.34 164x418x64.9 from 88.71 157x264 
1981 Sep 7    89.90 151x389x64.9 from 89.26 151x325 
1981 Sep 9    89.84 177x358x64.9 from 89.56 147x358 
1981 Sep 16    89.93 194x348x64.9 from 89.21 167x304 
1981 Sep 23    89.82 188x342x64.0 from 89.13 175x289 
1981 Oct 2    88.66 166x250x64.9 
1981 Oct 2 2231? Landed after 43d

Aviation Week: February 21,2005

 https://welib.org/md5/874c490d7a3550433e356bea20a91057

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