Saturday, June 29, 2002

RHESSI

 2002-004A


The High Energy Solar Spectroscopic Imager, in the SMEX series, studies particle acceleration in solar flares. Launch in 2002 by Pegasus XL after many delays.

HESSI rotates at 15rpm, imaging hard X-rays by reconstructing Fourier components from the time modulation of the flux through a set of 9 grids each 9cm in diameter. Angular resolution will be 2 arcsec at 40 keV and 36 arcsec at 1 MeV, and effective area is 100 sq cm. HESSI will also be used to image the Crab Nebula.

The first extrasolar observations were reported in April 2002. SGR 1900+14 was observed from 25 to 400 keV; an unusually bright 3-hour burst of Cygnus X-1 was detected on 2002 Feb 24. RHESSI will search for the electron/positron flash from novae; it has a much larger field of view than the Integral instruments.

Mass is 304 kg. Size is 1.1m dia 2.2m long. 5.7m span. 0.45m grid support cylinder, 9 x 9cm grids. Cylinder + box + 4 panels. Orbit 600 x 600 x 38.

Final stage is 0.97dia 1.34l and mass 202 kg.

The spacecraft was damaged when a vibration test in Mar 2000 was carried out at 20g instead of 2g

Bus is Spectrum Astro SA200S?, later Orbital Leostar-1. (or 3?)

Launch is from 28.0N 78.5W after takeoff from CCAFS Skid Strip. Drop 120km E of Palm Bay.

HESSI was renamed the (Reuven) Ramaty High-Energy Solar Spectroscopic Imager, or RHESSI, in Mar 2002. Ramaty, who died in 2001, was involved in the early stages of the project.


RHESSI 
 

DateTimeEventOrbit  

2002 Feb 5 1929  T/O from Skid Strip RW30/12 
 2058:12  Drop 
 2058:17  T+0:05 St 1 burn 
  T+1:15 St 1 burnout 
  T+1:31 St 2 burn 
  T+2:06 Fairing sep
  T+2:43 St 2 burnout 
 2105:46  T+7:34 St 3 burn 68s 
 2107:00  T+8:42 St 3 burnout 
 2108:00  T+9:42 St 3 sep 

Payload:

  • Rotating modulation collimator transform telescope

  • Ge crystal solid state spectrometer, 3 keV - 20 MeV, 1 keV res

Progress M-33

 1996-066A


Progress M-33 (11F615A55 No. 233) was launched in Nov 1996. Launch mass was 7190 kg. In the approach to re-dock at the +X port on Mar 3, the crew were planning to use the TORU system but could not get a TV picture from Progress; the re-docking was cancelled. Progress was deorbited over the Pacific on Mar 12.


Progress M-33 
 

DateTimeEventOrbit  

1996 Nov 19  2320:38  Launch by Soyuz-U  KB LC1 
 2322:36  Blok BVGD sep T+1:58 
 2325:25  Blok A sep T+4:47 
 2329:27  Blok-I sep T+8:49 
1996 Nov 20  0037   88.5 192 x 252 x 51.6 (AVM) 
 0206   88.5 191 x 252 x 51.6 (AVM) 
 0229:06  TCM 1  
 0347:59  TCM 2, 45s  90.0 255 x 305 x 51.6 (AVM)  
1996 Nov 22  0101:30  Docked with Mir +X 
1997 Feb 6  1213:56  Undocked Mir +X 
1997 Feb 7    377 x 395 x 51.65 
1997 Mar 3  0822:20  TCM 2  370 x 406 x 51.6 (AVM) 
1997 Mar 4  0510:29s  TCM 3 
 0557:12s  TCM 4 
 0701:34s TCM 5 
 0740 Failed to dock 
1997 Mar 12  0235:00 Deorbited 178s; mass 5592 kg 
 0323:37 Reentered over S Pacific 42.343S 140.482W

Friday, June 28, 2002

ICO F1

 2000-F02


The first ICO Global Communications satellite was lost when its Zenit-3SL launch vehicle failed on Mar 12. ICO F-1 was a 2750 kg Hughes HS-601M satellite and would have entered a 10300 km x 45 deg circular orbit. The Zenit-3SL vehicle took of from Boeing Sea Launch's Odyssey platform in the Pacific at 154W 0N. The second stage shut down 7 min into flight because of a prelaunch commanding error in the vernier system, A second stage valve remained open and by the time of ignition had lost more than 60 percent of its pressure. The satellite fell in the South Pacific, possibly south of Pitcairn. ICO's satellites carry multiple spot beams for mobile communications.

The satellite fell in the ocean 4300 km from the launch site in the S Pacific, perhaps around 25S 130W.

Planned orbit was 10390 x 10390 x 45. Presumably MECO-1 orbit was planned to be around 200 x 10390 x 40.


ICO 1 
 

DateTimeEventOrbit  

2000 Mar 12  1449:15  Launch by Zenit-3SL  SLO 
  T+2:25 St 1 sep, St 2 burn 
  T+2:58 Fairing 
 1456 T+7:41 St 2 premature MECO 
 1458 T+9:04 St 2 sep 
 1502 T+13:00? Apogee 200 km 

Raduga 1

  1975-123A


Raduga 11F638 No. 11L was launched on 1975 Dec 22 from Baikonur as the USSR's first operational geostationary comsat. It carried C-band transponders.


Raduga 1
 

DateTimeEventOrbit  

1975 Dec 22  1300 Launch by Proton-K  KB 
 1309 Stage 3 MECO  146 x 198 x 51.5 
 1417? Blok-DM burn 1  278 x 35676 x 47.3  
 1933? Blok-DM burn 2 
 1937? Blok-DM sep 
1975 Dec 24   
1975 Dec    GEO 85E? 
1978 Mar 31    1436.02 35704 x 35865 x 1.5 GEO 85.6E+0.01E 
1978 May 1    1436.12 35706 x 35867 x 1.6 GEO 85.8E+0.01W 
1978 Aug 5    1436.37 35764 x 35819 x 1.7 GEO 81.8E+0.08W 
1978 Oct 31    1436.46 35769 x 35827 x 1.9 GEO 74.5E+0.1W 
1991 Aug 27    1436.07 35760 x 35812 x 11.8 GEO 64.3Edr 
1999 Apr 26    1436.42 35782 x 35803 x 15.0 GEO 78.7Ed

Wednesday, June 26, 2002

Telstar 402

 1995-049A


Telstar 402 was launched on 1995 Sep 24 by Ariane from Kourou. The third stage of the Ariane 42L was an H-10+ model, dry mass 2079 kg including the equipment bay. Launch mass of Telstar 402R was 3410 kg; BOL mass was 2097 kg and dry mass is 1578 kg. The spacecraft bus was 2.2 x 2.5 x 4.0 m with a 24.5m span. The satellite was to provide C/Ku band services to the USA, Puerto Rico and the US Virgin Islands from GEO 89W.


Telstar 402
 

DateTimeEventOrbit  

1995 Sep 24  0006  Launch by Ariane 42L (V78)  CSG ELA2 
 0008  PAL sep (T+2:30) 
 0009  Stage 1 sep (T+3:10)
 0009  Stage 2 MES (T+3:30) 
 0010  Fairing 01 sep (T+4:00) 
 0011  Stage 2 sep (T+5:23) 
 0011  H-10+ Stage 3 MES (T+5:28) 
 0024  Stage 3 cutoff (T+18:27) 
 0026  Telstar 402R/stage 3 sep (T+20:24)  
 0029  V78 mission complete 
1995 Sep 24    631.92 273 x 35756 x 6.9 
1995 Sep 25  1300? LAM-1 
1995 Sep 26    720.40 4744 x 35739 x 4.3 
1995 Sep 26  1300? LAM-2 
1995 Sep 27    866.65 11751 x 35714 x 2.3 
1995 Sep 27  1800? LAM-3 
1995 Sep 27    1414.99 35014 x 35730 x 0.2 
1995 Sep 29  2300? mv in 
1995 Oct 1    1435.57 35726 x 35826 x 0.2 GEO 89.1W+0.1E 
1995 Oct 3   On station  GEO 89.1W 
1997 Jan 20    1436.13 35780 x 35793 x 0.0 GEO 89.0W 
1999 Oct 15    1436.11 35778 x 35795 x 0.1 GEO 89.0W 

OAO 1

  1966-031A


The OAO A1 satellite was launched at 1935 on 1966 Apr 8 by an Atlas Agena D. At 2035 it entered a 100.7 min, 792 x 806 km x 35.0 deg orbit, becoming Orbiting Astronomical Observatory 1. OAO I successfully demonstrated the use of star trackers for accurate attitude control, but on Apr 10 its battery failed and the satellite fell silent.

The spacecraft had a hinged optics cover; it's not clear if this was opened prior to failure. One piece of debris with RCS 2.6 sq m separated at the time of failure; possibly there was a minor explosion in the battery, or a structural failure after loss of attitude control.


OAO 1 
 

DateTimeEventOrbit  

1966 Apr 8  1935:00  Launch by Atlas Agena D  CKAFS LC12 
 1937:16 T+2:16 BECO 
 1939:25 T+4:25 SECO 
 1939:30 T+4:30 Fairing sep 
 1939:45 T+4:45 VECO 
 1939:47 T+4:47 Atlas sep 
 1940:38 T+5:38 Agena 6703 MES-1 
 1944:33 T+9:33 Agena MECO-1  94.07 159 x 802 x 35.0 
 2034:06 T+0:59:06 Agena MES-2 6s 
 2034:12 T+0:59:12 Agena MECO-2  100.8 791 x 804 x 35.0 
 2034:40  T+0:59:40 Solar arrays  
 2035:05  T+1:00:05 Solar booms deploy  
 2035:45 T+1:00:45 Agena sep 
 2302  Battery temp high  
1966 Apr 10  0014  Command tumble to cool battery 
1996 Apr 10  0207  Battery 1 depleted 
 0552  Battery 2 and 3 depleted, spacecraft failed 

Payload:

  • WEP Wisconsin Experiment Package with 1100-3000A UV telescopes:

  • 20-cm stellar telescopes (4)

Tuesday, June 25, 2002

Molniya 351

 2001-030A


The first Molniya-3K, launched on 2001 Jul 20, was designated Molniya-3. Some initial confusion reported it incorrectly as Molniya-1K. Mass is 1780 kg.


Molniya-3K 
 

DateTimeEventOrbit  

2001 Jul 20  0017  Launch by 8K78M PL LC43/4 
 0026  Blok-I MECO 
 0026  Blok-I sep  90.87 214 x 420 x 62.82  
 0109? Blok-ML burn 
 0109? BOZ sep 
 0110? Blok-ML MECO 
 0111 Blok-ML sep 
2001 Jul 22  1359   735.79 407 x 40831 x 62.9 
2001 Jul 26    735.87 419 x 40823 x 62.9 
2001 Jul 27   TCM 
2001 Jul 31    706.94 428 x 39390 x 62.9 
2001 Aug 8    717.79 443 x 39911 x 62.9 
2001 Sep 4    717.85 487 x 39870 x 62.9 
2002 May 19    717.73 462 x 39889 x 64.1

STS-50 (Columbia)

 1992-034A


STS-50 was launched on 1992 Jun 25. It was the first flight with the EDO cryogenics pallet to provide extra electrical power and oxygen, supporting the USML-1 Spacelab mission. The first landing attempt on Jul 8 at Edwards was waved off due to bad weather.

The USML included a crystal growth facility capable of processing samples up to 1850K. The Drop Physics Module studied coalescence of fluid drops and a compound drop with one fluid inside another. A new `glovebox' mini-laboratory was used for fluid physics and crystal growth experiments.


STS-50 
 

DateTimeEventOrbit  

1992 May 29   Rollover  VAB/3 
1992 Jun 3   Rollout  LC39A 
1992 Jun 25  1612:22  Launch  LC39 
 1614:29  SRB sep 
 1620:51  MECO  68 x 304 x 28.5 
 1621:08  ET sep 
 1652:14  OMS 2 2:22 68m/s  90.60 299 x 307 x 28.46 
 1654:35  OMS-2 CO 
 1738  PLBD open 
 2042  SL activate 
1992 Jun 26  0200   90.57 299 x 305 x 28.47 
 0615EDO supply activate 
1992 Jul 29  0416   90.56 299 x 304 x 28.47 
 1250?  RCS orbit adjust 
1992 Jun 29  2219   90.47 293 x 301 x 28.47 
1992 Jul 5  1345   90.49 293 x 303 x 28.47 
1992 Jul 8  0328   90.50 293 x 304 x 28.47 
1992 Jul 8  0929  PLBD close 
 1055Waveoff WX 
 1210PLBD open 
 1509:22  OMS-3 31s 15m/s, adjust track 
 1509:53  OMS-3 CO 
1992 Jul 8  1830   89.98 245 x 301 x 28.47 
1992 Jul 9  0804  PLBD close 
1992 Jul 9  1041:38  OMS DO 3:24 104m/s 89.97 245 x 299 x 28.5 
 1045:02  OMS DO CO 
 1110:46  Entry 
 1142:11  Gear down 
 1142:27  Landing  RW 33 KSC 
 1142:44  NGTD 
 1142:44  Drag chute out 
 1143:13  Chute sep 
 1143:26  Wheels stop 
1992 Jul 10  1545
OPF/1 

May 13,2026

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