Monday, September 30, 2002

Yohkoh

 1991-062A


The Solar-A satellite was launched in Aug 1991. It was renamed Yohkoh (`Sunlight'). Yohkoh returned daily X-ray images of the Sun with the NASA soft X-ray telescope.

After 10 years in space, Yohkoh lost attitude control during a solar eclipse which happened at a time of poor ground communications; the batteries drained to a low state and the spacecraft is oriented in a way that keeps them cold. Yohkoh was decommissioned the following year.


Yohkoh 
 

DateTimeEventOrbit  

1991 Aug 30  0230  Launch by Mu 3S2  KASC 
  T+0:40 SOB sep 
  T+1:24 Stage 1 cutoff, sep 
  T+1:26 Stage 2 start 
  T+2:36 Stage 2 cutoff, coast 
  T+2:35 Fairing 
 0233 T+3:15 Stage 3 spinup 
 0234 T+4:00 Stage 2 sep 
 0237 T+7:13 Stage 3 burn 87s? at 570 km 
 0238 T+8:40? M3B rocket cutoff 
 0239 T+9:30 M3B sep  
 0239 T+9:40 Yo-yo despin 
   520 x 770 x 31.3 
1991 Nov 20  97.87 522 x 791 x 31.3 
2001 Dec 14   Discharged batteries during eclipse 
2002 Jun   end of ops 

Payload:

  • HXT Hard imaging XR telescope ISAS 10-100 keV, 8" res. (Fourier synthesis telescope; 64 PMT array )

  • SXT Soft imaging XR telescope NASA-MSFC/LPARL 2" resolution 0.25 - 4 keV, 4-50A, 1.6m focal length Nariai-Werner, with CCD. Aperture 1 cm?

  • BCS Bragg crystal spectrometer ISAS/UK; 1.8-5A

  • WBXS Wide band soft X spectrometer ISAS 2 keV - 100 MeV.

Tales from the Prom

 https://welib.org/md5/89989c6bd84cf79735f9e3d22bbfdbc7

Thursday, September 26, 2002

Uosat

 1999-021A


Uosat is a 325 kg Minisat-400 from SSTL. The imaging payload includes a wide angle camera, a high res camera, and multispectral cameras. The satellite has a gravity gradient boom but it was not deployed since momentum wheels were used instead.

Launch 1999 Apr 21 by Dnepr RS-20K (RS-20 based). The R-36MUTTKh (RS-20) can have an S5M or Fregat third stage but on this flight was a minimally modified two-stage vehicle with a post-boost third stage. Uosat 12 was placed in circular orbit together with a fairing part, following which the post-boost stage made a depletion burn to enter eccentric orbit.

Dnepr is marketed by ISC Kosmotras/Kiev. It can launch 3000 kg to 500 km. NK9903 says it's based on 15A14 R-36M not 15A18M R-36M2 but NK9906 says it's 15A18 (R-36M1).

N2O4/UDMH stages, stage 2 is RD-0256 by KBKhA.  


UoSAT 
 

DateTimeEventOrbit  

1999 Apr 21  0459:12  Launch by Dnepr  KB PL108 
 0500:58  T+1:46 Stage 2 VES 
 0500:59  T+1:47 Stage 1 MECO 
 0501:02  T+1:50 Stage 1 sep 
 0501:05  T+1:53 Stage 2 MES 
 0503:38  T+4:26 Stage 2 MECO 
 0503:48  T+4:36 GO sep 
 0503:53  T+4:41 Stage 2 VECO 
 0503:56  T+4:44 RS burn  
 0510  T+11:40 control to Gol-2 
 0513:47  T+14:35 Plume shield sep 
 0513:48  T+14:36 Uosat sep 638 x 652 x 64.6 
 0514:48  T+15:36 Stage 3 RS cutoff 599 x 1403 x 64.6 
1999 Jul 2   Begin cold gas test 
1999 Jul 7?  120s burn, 0.2km height adjust 
2001 Jan   HTTP server test from space 

Friday, September 20, 2002

ERS-2

 1995-021A


The ERS-2 satellite was similar to ERS-1. With a mass of 2700 kg, it was made by Daimler-Benz/Dornier. It included a 12 m solar array and a 10-m SAR radar attached to the standard SPOT class bus. The main new instrument was an ozone monitor with improved capability for global ozone monitoring.


ERS-2 
 

DateTimeEventOrbit  

1995 Apr 21  1344  Launch by Ariane 40+ (V72)  CSG ELA2  
  Stage 1 L220 sep (T+2:39?) 
  Fairing 01 sep (T+3:48?) 
  Stage 2 L33 sep (T+4:48?) 
  Stage 3 ignite (T+4:53?) 
 1400?  Stage 3 cutoff (T+16:44?) 
 1401? Stage 3 sep 
1995 Apr 21    100.56 783 x 786 x 98.6  
1995 Apr 24    100.34 773 x 776 x 98.6 
1995 Apr 27    100.53 774 x 793 x 98.6 
1998 Jan 4  100.54 783 x 785 x 98.6 
2000 Jul 15   100.54 782 x 785 x 98.6 

Wednesday, September 18, 2002

Kosmos 424

  1971-048A


Kosmos-424 was launched in May 1971 from Plesetsk and flew a 13 day mission.


Kosmos-424 
 

DateTimeEventOrbit  

1971 May 28  1030:00  Launch by 11A57  PL 
 1034  Blok-I burn  
 1038 Blok-I sep 
1971 May 30  0657   89.35 198 x 286 x 65.4 
1971 May 30  1430   89.36 204 x 282 x 65.40 (RAE)  
1971 May 31  1411   89.34 195 x 287 x 65.4 
  Orbit change 
1971 Jun 1  1358   89.37 174 x 312 x 65.4 
1971 Jun 7  2148   89.25 175 x 298 x 65.4 
1971 Jun 9  1200?  Engine sep
1971 Jun 10  0316? Retrofire 
 0326?  PO sep 
 0331? Entry 
 0347? Landed after 12.71d 

Apollo 13 (Odyssey)

  1970-029A


Apollo CSM 109 was assigned to Apollo 13, the third attempted landing mission, and named Odyssey. It was paired with LM 7 Aquarius.

At 0306 on Apr 14, the command to stir the cryo tanks was given; within a minute, an electrical fire had begun in Sector IV of the Service Module. At 0307:53 the fire caused Oxygen Tank No. 2 to explode; the side of the SM covering Sector IV was blown away and the CSM lost its electrical power, its oxygen supply, its water supply, and possibly its propulsion capability. The crew were 330000 km from Earth on a trajectory which threatened to strand them in space. The spaceship shook with a loud bang, and RCS jets fired to regain stability. Houston initially suspected erroneous readings, but as the crew saw their precious oxygen venting into space the seriousness of the situation became clear....


Odyssey (CSM 109) 
 

DateTimeEventOrbit  

1970 Apr 11  1913:00  Launch by Saturn V (SA-508)  KSC LC39A 
 1915:15  S-IC CECO 
 1915:44  S-IC OECO, S-IC sep 
 1915:46  S-II ignition 
 1916:14  Interstage sep 
 1916:20  LES sep 
 1918:31  S-II premature CECO 
 1922:53  S-II OECO, sep 
 1922:57  S-IVB ignition 
 1925:30  S-IVB cutoff 
 1925:40  Earth orbit insertion  88.32 184 x 198 x 32.6 
 2148:46  S-IVB TLI burn 
 2154:37  S-IVB cutoff 
 2154:47  Translunar injection 217 x 566793 x 31.81  
 2219:39  CSM sep from S-IVB/SLA  219 x 549183 x 31.74  
  SLA panels sep 
 2221  At 24m 
 2230  CSM docked with LM 
 2232  CSM hard docked 
 2314:03  CSM/LM sep from S-IVB 
1970 Apr 12  1215?  Pass h4 = EL1:4  
1970 Apr 13  0153:50  MCC-2 burn, hybrid trajectory  
 0153:53  MCC-2 CO  -146 x 553315 x 31.8  
1970 Apr 14  0119  CDR and LMP to LM 
 0300  CDR and LMP return to CM 
 0306  SM cryo tank stir 
 0307  Electrical fire in SM Sector IV 
 0307:53  Explosion in Sector IV 
 0451  LM transfer hatch open 
 0551  CM power down, crew transfer to LM 
 0906?  Equigravisphere 
1970 Apr 17  1123  CM power up, crew transfer to CM 
 1315  SM-109 jettison  41 x 836791 x 30.6 
 1600  LM hatch closed 
 1643:02  Undocked from LM  41 x 836196 x 30.6 
 1753:47  Entry  43 x 947783 x 30.8 
 1807:41  Splashdown 21 40S 165 22W Pacific 
  Recovered by USS Iwo Jima 

Soyuz 30

 1978-065A


Spacecraft 11F615A9 No. 67 was left over from the Almaz OPS 3 program. With no prospect for a near term Almaz 4 mission, it appears to have been converted for use as a DOS ferry. It was launched in June 1978 as Soyuz-30 and docked with the rear port of DOS 5 (Salyut-6) the following day. Soyuz-30 carried veteran Soviet astronaut Pyotr Klimuk and the first Polish astronaut, Miroslaw Hermaszewski.


Soyuz-30 
 

DateTimeEventOrbit  

1978 Jun 27  1527:21  Launch by Soyuz-U  KB 
 1529 Blok BVGD sep 
 1532  Blok A sep 
 1536  Blok I MECO 
 1536  Blok I sep 
   88.8 194 x 244 x 51.6 
1978 Jun 28  1300  TCM  264 x 310 x 51.6 
 1708  Docked with DOS 5 +X port 
 2010  Hatch open 
1978 Jul 5  1015  Undocked 
 1139  Landing program on 
 1242? Retrofire 
 1245? DO CO 
 1300?  Modules sep 
 1306?  Entry 
 1330:20  Landed 300 km W of Tselinograd

Tuesday, September 17, 2002

Skynet 4A

 1990-001A


The Skynet 4 series were built by British Aerospace and Marconi, using the ECS bus.


Skynet 4A 
 

DateTimeEventOrbit  

1990 Jan 1  0007  Launch by Commercial Titan 3  CC LC40 
 0008:49  Stage 1 ignition 
 0009  SRM sep 
 0011:27  Stage 2 ignition 
 0011:38  Fairing sep 
 0015:06  Stage 2 shutdown  165 x 612 x 28.6 
 0118:52  Skynet 4A deployed 
 0205?  PAM-D2 burn to GTO 
 0207? PAM-D2 burnout 
 0210? PAM-D2 sep 
 0830? Apo 1 over 58E 
 1230? Peri 1 
 1900? Apo 2 over 96W 
 2230? Peri 2 
1990 Jan 2  0500? Apo 3 over 110E 
 0900? Peri 3 
 1500? Apo 4 over 42W 
 1900? Peri 4 
1990 Jan 3  0044?  AKM burn over 167E  
 0130? Apo 5 over 162E 
1990 Jan 3    1380.42 33675 x 35703 x 3.4 GEO 170.1E+14.5E 
1990 Jan 10   1382.67 33673 x 35794 x 3.4 GEO 80.8W+13.9E 
1990 Jan 16    1419.99 35133 x 35808 x 3.4 GEO 42.1W+4.1E 
1990 Jan 20    1428.19 35453 x 35809 x 3.4 GEO 27.1W+2.0E 
1990 Jan 29    1427.54 35449 x 35788 x 3.4 GEO 7.8E+2.2E 
1990 Feb 17    1436.12 35781 x 35793 x 3.4 GEO 6.0E 
1990 Dec 10    1436.03 35652 x 35918 x 2.7 GEO 6.2E 
1990 Dec 26   mv out 
1991 Jan 11   mv in  1436.00 35731 x 35838 x 2.7 GEO 29.5E 
1991 Mar 24    1436.03 35769 x 35800 x 2.6 GEO 29.5E 
1991 Jun 20    1435.99 35732 x 35836 x 2.4 GEO 29.6E 
1991 Jul 7    1436.03 35497 x 36073 x 2.5 GEO 29.2E 
1991   Move to 65E? 
1991 Oct 4    1435.71 35625 x 35932 x 2.8 GEO 65.4E+0.1E 
1991 Oct 14    1435.73 35620 x 35738 x 3.0 GEO 65.6E 
1991   Move to 34W 
1992 Jan 3    1436.00 35771 x 35797 x 2.2 GEO 34.0W 
1992 May 2    1436.12 35784 x 35789 x 2.0 GEO 34.0W 
1994 Apr 30    1436.15 35774 x 35800 x 1.7 GEO 34.1W 
1997 Oct 15    1436.12 35772 x 35801 x 3.0 GEO 34.0W 
1999 Jun 16    1436.09 35782 x 35791 x 3.8 GEO 34.0W 
2000 Sep 5    1436.11 35774 x 35798 x 5.6 GEO 34.5W 

Sunday, September 15, 2002

Kosmos 670

  1974-061A


The first of the new Soyuz class was 11F732 No. 1L, or 7K-S No. 1L. It was launched on an unpiloted test flight on 1974 Aug 6, into an unprecedented 50.6 degree inclination orbit, and recovered 3 days later. The craft was given the cover name Kosmos-670. The reentry was ballistic rather than lifting because of a problem at module separation. 


Kosmos-670 
 

DateTimeEventOrbit  

1974 Aug 6  0002:00 Launch by Soyuz  KB 
 0004  Blok BVGD sep 
 0006  Blok A sep 
 0010  Blok I MECO 
 0010  Blok I sep 
1974 Aug 6  89.51 209x292x50.57 
1974 Aug 7  89.51 209x292x50.57 
1974 Aug 8  89.46 210x286x50.55 
1974 Aug 9  0044? DO 80m/s
 0048?  DO CO 
 0100?  PAO sep 
 0108?  Entry  
 0130 Landed 

Sunday, September 8, 2002

Intelsat 4A2

  1976-010A


Intelsat 4A F2 was launched in Jan 1976 and became the AOR Primary Spare.


Intelsat IVA F-2 
 

DateTimeEventOrbit  

1976 Jan 29  2356  Launch by Atlas Centaur  CC LC36 
 2358  Booster sep
1976 Jan 30  0000  Atlas sep 
 0000:18? MES-1 
 0000:30? Fairing 
1976 Jan 30  0006:21? T+10:21 Centaur MECO  184? x 1800? x 28.1? 
 0020:30? MES-2 2:05 
 0022:35? MECO-2 
1976 Jan 30  0024  Centaur sep, Orbit insertion  578 x 36749  
  
  Centaur venting 
 0630?  Apo 1 
 1700? Apo 2 
1976 Jan 31

 

0300? Apo 3 
 1400? Apo 4 
1976 Feb 1  0019  Apo 5, SVM-4A burn? 
1976 Feb 1  0219  Apo 5, SVM-4A burn, over W POR 

1976 Feb 2  

  GEO 140E +3E/d 
   1420.2 35084 x 35869 x 0.11 (Fal) 
1976 Feb   AOR Primary Spare  GEO 29.5W 
1977 Jan 21    1436.15 35779 x 35796 x 0.0 GEO 29.6W+0.0 
1978 May 25    1436.07 35781 x 35791 x 0.0 GEO 29.5W 
1979 Jul 19    1436.11 35781 x 35792 x 0.0 GEO 29.5W+0.01W 
1979 Jul 21   mv out 1435.82 35766 x 35785 x 0.1 GEO 28.9W+0.06E 
1979 Aug 14   mv in 1436.15 35779 x 35796 x 0.0 GEO 27.4W+0.02W 
1979 Sep   Domestic Lease, contingency GEO 27.5W 
1980 Jan 14    1436.13 35774 x 35799 x 0.0 GEO 27.5W+0.02W 
1980 Oct 12    1436.10 35777 x 35795 x 0.0 GEO 27.4W+0.0W 
1980 Oct 22    1436.13 35777 x 35796 x 0.0 GEO 27.5W+0.02W 
1980 Nov?   Move to 21.5W 
1980 Dec 2    1436.17 35778 x 35798 x 0.0 GEO 21.7W+0.03W 
1981 Jan 2    1436.08 35776 x 35796 x 0.1 GEO 21.4W+0.0W 
1981 Jun 11   AOR Major Path 2  GEO 21.5W 
1981 Oct 2    1436.15 35778 x 35796 x 0.3 GEO 21.5W+0.02W 
1982 Dec 18  Domestic lease/contingency  1436.13 35779 x 35794 x 0.0 GEO 21.5W 
1983 Feb 21    1436.16 35783 x 35790 x 0.0 GEO 21.6W+0.01W 
1983 Feb 21   mv out  
1983 Mar 30    1436.16 35775 x 35800 x 0.2 GEO 56.9E+0.02W 
1983 Apr   IOR domestic lease/contingency  GEO 57E 
1983 Jun 1    1436.15 35774 x 35800 x 0.0 GEO 57.0E+0.02W 
1984 Jan 11    1436.10 35783 x 35790 x 0.1 GEO 56.9E+0.0W 
1984 Jan 17   mv out  
1984 Mar 21    1438.08 35780 x 35870 x 0.3 GEO 46.8E+0.5W 
1984 Aug 4    1437.25 35751 x 35867 x 0.6 GEO 2.8W+0.3W 
1984 Aug   mv in, AOR Spare  GEO 4W 
1984 Aug 17    1436.20 35749 x 35827 x 0.6 GEO 4.0W+0.03W 
1984 Oct 1    1436.14 35750 x 35825 x 0.8 GEO 4.9W+0.02W 
1985 Jan 13    1435.99 35759 x 35810 x 1.0 GEO 4.1W+0.02E 
1985 Mar 15    1435.91 35755 x 35810 x 1.2 GEO 1.5W+0.04E 
1985 Apr 13    1436.12 35761 x 35813 x 1.2 GEO 2.1W+0.01W 
1985 Nov 27    1436.05 35759 x 35812 x 1.8 GEO 1.9E+0.0E 
1985 Dec 19   orbit raise 1443.60 35910 x 35956 x 1.9 
1987 Mar 1    1444.43 35925 x 35973 x 3.0  
1990 Nov 25    1444.41 35930 x 35967 x 6.5 
1995 Nov 24    1444.57 35924 x 35980 x 10.3 
1999 Apr 28    1444.42 35941 x 35957 x 11.9

These Are Not My Beautiful Stories

  Summary: The chapters within are outlines for both future stories I’ve got planned (in the case that I never get around to writing them) a...