Wednesday, February 28, 2001

STS-78 (Columbia)

 1996-036A


The STS-78 mission carried the LMS (Life and Microgravity Sciences) Spacelab and the EDO Extended Duration Orbiter kit. Commander Tom Henricks led a crew including pilot Kevin Kregel, payload commander Susan Helms, vet Richard Linnehan, doctor Charles Brady, CNES astronaut Jean-Jacques Favier and Canadian astronaut Robert Thirsk. For the first time, a camera in the cabin recorded the ascent. A minor hardware problem surfaced in the backup flight system, but the launch appeared otherwise uneventful. However, the ET ran out of hydrogen instants before SSME shutdown - the engines completed the burn using the last fuel in the propellant lines, narrowly avoiding a possible catastrophic event in the SSMEs (https://waynehale.wordpress.com/2014/10/08/understanding-sts-93-the-key-is-mixture-ratio/)

Also, after the SRB's were recovered and examined, it turned out that hot gas had slipped through the J-flange of the field joints. While it was stopped by the O-rings, this was the first time this had happened and caused some concern.

STS-78 was the first carried out under the auspices of the United Space Alliance as prime processing and launch contractor, replacing Lockheed Martin. USA was a joint venture between Lockheed Martin and Rockwell.

Problems with the Flash Evaporator System meant that the payload bay door radiators were deployed to lower the heat load on the system. The Bubble, Drop and Particle Unit malfunctioned but was repaired on Jun 28. Halfway through the flight, approval was given for a record flight day 17. On Jul 6, the astronauts tested a method for raising the orbital altitude using only the vernier jets. The technique was being developed to allow gentle reboost of the Hubble Space Telescope without the need to retract its solar arrays. Columbia returned to KSC on Jul 7 after a record breaking mission.


STS-78 
 

DateTimeEventOrbit  

1996 May 21   Transfer from OPF to VAB  
1996 May 22   ET mate 
1996 May 30   Roll to LC39B 
1996 Jun 20  1449:00  Launch by STS  KSC LC39B/MLP-3 
 1451:03  SRB sep 
 1457:30  MECO 
 1457:49  ET-79 sep  88 x 282 x 39.0 (OMS dV) 
 1530:28  OMS-2, 1:57 56.4 m/s  
 1532:26 OMS-2 CO  
 1609  PLBD open 
 1655Go for orbit ops 
 1915RCS orbit adjust 52s 4m/s 

2200 90.12 278 x 282 x 39.02 
1996 Jun 21  0600   89.97 267 x 278 x 39.02 
1996 Jun 22  1813  Port radiator deployed 
1996 Jun 24  0600   89.92 265 x 275 x 39.02 
1996 Jun 26  0600   89.91 265 x 274 x 39.02 
1996 Jun 27  0600   89.89 264 x 273 x 39.02 
1996 Jun 28  0600   89.87 263 x 272 x 39.02 
1996 Jul 1  0600   89.81 260 x 269 x 39.01 
1996 Jul 3  0600   89.77 259 x 267 x 39.01 

1704  Starboard radiator deployed 
1996 Jul 5  0630   89.76 258 x 265 x 39.01 
1996 Jul 6  0300   89.74 257 x 264 x 39.0 

1011  RCS vernier orbit adjust, 5 min  89.58 246 x 261 x 39.0  
1996 Jul 7  0850  PLBD closed  89.58 246 x 260 x 39.0 
 0900:26 PLBD latched 
 1136:36  OMS DO 2:42 82.6 m/s  -30 x 260 x 39.0 
 1139:18  OMS DO CO  
 1204:37  Entry interface 
 1236:36  Landed at KSC RW33 (16:21:47:36) 
 1236:48  NGTD 
 1237:31  WS 

1630Towed to OPF/1 

DM-F3

 2000-048A


The Delta Mission Flight 3 payload is a mass model (instrumented payload simulator) of the Orion 3 HS-601 satellite. Launch Aug 2000. DM-F3 is a 2.04 dia 1.72m high 4348 kg cylinder. It is not designed to operate after separation from the second stage.

DM-F3 will be used by the USAF as a passive calibration satellite for study of payload dynamics and thermal state in orbit. The outer surface is painted with black and white stripes and reflective surface were added to provide laser targets.

In the event the orbit reached was significantly low compared to that planned.


DM-F3 
 

DateTimeEventOrbit  

2000 Aug 23  1105:00 Launch by Delta 8930  CC LC17B 
  T+1:17 SRM 1-6 out 
  T+1:19 SRM 7-9 on 
  T+1:20 SRM 1-6 sep 
  T+2:35 SRM 7-9 out 
  T+2:37 SRM 7-9 sep 
  T+3:45 Fairing sep
  T+4:19 MECO 
  T+4:27 St 1 sep  -4900 x 158 x 29.5 
  T+4:41 SES-1 
 1118 T+13:40 SECO-1  157 x 1363 x 29.50 (ILAM) 
 1126  T+21:55 SES-2 
 1129  T+24:38 SECO-2  183 x 25778 x 27.52 (ILAM) 
 1141  T+36:18 Stage 2 sep  186 x 25770 x 27.5 (ILAM) 
 1145s T+40:33 CCAM 
 1154s T+51:12 depletion   188 x 25768 x 27.6 (ILAM) 
  (B) 353.79 163 x 20219 x 27.9  
  (A) 345.95 51 x 19841 x 28.1 

Monday, February 26, 2001

Skynet 1A

  1969-101A


The Skynet 1 program was also called IDCSP/Augmentation and was considered to be related to the USAF's DSCS program. Skynet was sponsored by the UK Ministry of Defence in association with the Ministry of Technology. The satellite was built by Philco. SAMSO helped manage the program. USAF checked out the satellite on orbit and then transferred control to the RAF at Oakhangar.


Skynet 1A 
 

DateTimeEventOrbit  

1969 Nov 22  0037:00 Launch by Delta M  CK LC17A 
  T+0:39 SRM 1-3 out 
  T+1:10 SRM 1-3 sep 
 0040 T+3:38 MECO 
 0040 T+3:43 St 1 sep 
 0040 T+3:43 SES-1 6:17 
 0040 T+3:50 Fairing  
 0047:00 T+10:01 SECO-1 367 km 7.1667 km/s (rel?)  -1200? x 366  
 0059:54 T+22:52 St 2 sep 
 0100:07 T+23:06 TES 41.6s 339 km 
 0100:51 T+23:51 TECO 314 km 10.154 km/s 
 0102:32 T+25:32 St 3 sep  217 x 36629 x 27.2  
   655.3 258 x 37088 x 27.6 (MOR Post) 
1969 Nov 22  0530?  Apo 1 100E 
 1630? Apo 2 65W 
1969 Nov 23  0330?  Apo 3 130E 
 1430? Apo 4 35W 
1969 Nov 24  0130? Apo 5 160E 
1969 Nov 24  0139  Star 17A (TE-M-521) AKM burn 
1969 Nov    1407.8 34702 x 35838 x 2.4 
1969 Nov 25   (From Post MOR)  1431.01 34695 x 35754 x 2.44 
1969 Nov 25    1431.01 34695 x 36680 x 2.44 (TR-1022, MORP) 1.32E/d  
1969 Nov 26   TCM to 7.5E/d 
1969 Nov   1436.0 35799 x 35788 x 2.2 
1969 Dec    GEO 49E 
1970 Jan 7   Move into final orbit  GEO 39E 
1970 Jan 14    44E 
1970 Jan 19    1436.46 35791 x 35796 x 2.3 GEO 41.0E 
1970 Jan 30   Turned over to UK from SAMSO 
1970 Jun 15   At 50E, reverse drift to W 
1970 Aug 22   At 45E, begin E drift 
1970 Nov   At 50E, reverse drift 
1971 Jan   At 45E, begin E drift 
1971 May   At 50E, reverse drift 
1971 Jun   At 47E, begin E drift 
1972 Mar   End of regular operations 
1975 Dec 30    GEO 55E (Morgan) 
1977 Jun 24    1436.09 35697 x 35876 x 4.0 GEO 107.2W 
1980 Apr 5    1436.0 35897 x 35681 x 5.7 GEO 106.5W 
1980 Sep    1434.5 36827 x 34689 x 7.1 GEO 109W dr 
1989 Dec 27    1436.08 35699 x 35873 x 11.7 GEO 107.3W 
1990 Aug 31    1436.03 35686 x 35884 x 12.1 GEO 104.5W 
1992 Sep 9    1436.05 35681 x 35890 x 13.2 GEO 106.9W 
1994 Aug 26    1436.12 35680 x 35894 x 14.1 GEO 107.0W 
1996 Jul 25    1436.12 35686 x 35887 x 14.6 GEO 104.2W+0.01E 
1998 Jul 29    1436.08 35696 x 35876 x 14.7 GEO 103.4W 

Sunday, February 25, 2001

Kakehashi

 1998-011A


The Communications and Broadcasting Engineering Test Satellite is a NASDA experimental satellite using a modified Toshiba ETS 6 bus; system integrator for COMETS was NEC. COMETS will act as a data relay satellite for ADEOS, OICETS and ETS-7, as well as test mobile communications technology.  It will use Ka-band transmissions to support HDTV and digital broadcasting experiments and both Ka-band and mm-wave mobile communications.

COMETS was developed by NASDA and CRL/Tokyo. Launch drawings indicate the 4S fairing was used.

Launch was on 1998 Feb 21, but the orbit achieved was lower than planned. Initial planned transfer orbit was 250 x 35552 km x 28.5 deg, but NORAD tracked it in 247 x 1883 km x 30.0 deg. The second burn of the second stage cut off after only 44 seconds of the planned 3 min 12 sec burn when exhaust gases broke through the top of the engine nozzle due to a manufacturing flaw. Post-launch name was Kakehashi (`bridge' or `intermediary'). COMETS was tracked as object 25176 until Mar 23, then became object 25175.

COMETS had a Unified Propulsion Subsystem (UPS) with a 1700N apogee engine derived from LAPS. Unlike LAPS, UPS was an integral part of the COMETS satellite and included the RCS system which was separate on the earlier mission. After the failed launch, the UPS was used to raise the orbit of COMETS to 472 x 17715 km.

The IES engine was tested in early 1999 for a total of 14 hours.


COMETS 
 

DateTimeEventOrbit  

1998 Feb 21  0755  Launch by H-II-5/LAPS  TNSC Y 
  T+1:37 SRB sep 
 0759  Fairing sep T+4:00 
 0801  Stage 1 sep T+5:54 
 0801  Stage 2 burn 1, 304s 
 0806  SECO-1 802s coast 
 0818  T+23:26 Stage 2 burn 2 
 0819  cutoff at 44s  106.51 247 x 1883 x 30.0 
 0822s  COMETS sep 
1998 Mar 8  1745   106.45 248 x 1876 x 30.0 
1998 Mar 20  2210? LAPS-1  397 x 2493 x 30.0 
1998 May 6   LAPS burn 
1998 May 8    132.32 435 x 4011 x 30.0 
1998 May 26    201.25 463 x 9533 x 30.0 
1998 Jun 1    319.20 472 x 17715 x 30.0 
1999 Feb 26   Ion engine test 
1999 Mar 8   end of IES tests 
1999 Aug 6    318.91 479 x 17688 x 30.1 

Thursday, February 8, 2001

Aviation Week: October 16,2000

 https://welib.org/md5/7c233507ab72e0d79b5bc5a40566135d

Seventeen: January 2001

 https://welib.org/md5/3b81eff9aa61ad97f36b770fea51641b

Interbol 1

 1995-039A


SO-M2 no. 512 (Prognoz-M2) was launched in Aug 1995 and named Interbol-1. The satellite was also known as the Khvostovoy Zond (Interball Tail Probe), for exploration of the magnetotail. The 1250 kg probe carried a 50 kg Magion subsatellite. This was the first Prognoz launch from Plesetsk.


Prognoz-M2 No. 512 
 

DateTimeEventOrbit  

1995 Aug 2  2359:11  Launch by Molniya-M  PL LC43/3 
1995 Aug 3  0004:03  Blok-I MES 
1995 Aug 3  0008  Blok-I shutdown 
1995 Aug 3  0008:07  Blok-I sep  95.0 240 x 827 x 62.8 
1995 Aug 3  0100:30  T+1:01 Blok-2BL ignite 
1995 Aug 3  0101:10  T+1:02 BOZ sep 
1995 Aug 3  0104:15  T+1:05 shutdown
1995 Aug 3  0104:15  Blok-2BL sep  505 x 193064 x 63.8 
1995 Aug 3  0925?  Magion-4 sep 
 1945  Pass EL1:4 
1996 Aug 13  1400   12708 x 180145 x 69.02 (IPM) 
2000 Oct 16  0335  end of tx
2000 Oct 281403:33  Reentered over 10.99S 0.18E 
 

Payload:

  • SKA-1 3-D distribution of Ions 0.05-5 keV; energy spectra of antisolar ions 5-40 keV.

  • ELEKTRON 3-D dist. of 0.01-26 keV electrons.

  • PROMICS-3 Ion composition and energy distribution

  • VDP Fast measurements of ion or electron fluxes and directions.

  • AMEI-2 Energy spectra of ions

  • MONITOR 3 High time resolution solar wind ion fluxes and distributions.

  • CORAL Angular ion energy distributions, 0.05-25 keV

  • ALPHA-3 Thermal plasma ion flux

  • OPERA Electric field waves 0-50 kHz

  • MIF-M Magnetic field waves 0-64 Hz, 1-40 kHz.

  • IFPE Ion and electron flux fluctuations.

  • ADS Current fluctuations; Nine channel spectral analyser and cross correlator.

  • FGM-1 Magnetic field waves.

  • FM-31 Magnetic field.

  • AKR-X Radioemission in range 0.1-1.5 MHz.

  • SKA-2 Charged energetic particles composition and anisotropy.

  • DOK-2 Energy spectra, angular and time variations of electrons and ions.

  • RF-15-1 Solar X-ray burst spectra and time profile measurements, 2-240 keV

Wednesday, February 7, 2001

Kosmos 2319

 1995-045A


Kosmos-2319 was launched by Proton on 1995 Aug 30. The Geizer comsat was stationed at 80 deg E, replacing Kosmos-2291.


Kosmos-2319 
 

DateTimeEventOrbit  

1995 Aug 30  1933  Launch by Proton-K/DM2 KB 
 1938  Stage 3 burn 
 1942  Stage 3 sep  190 x 195 x 51.7 
 2040?  DM burn 1 
1995 Aug 31  0100?  DM burn 2 
 0120?  DM sep 
1995 Aug 31    1441.02 35806 x 35959 x 1.5 GEO 90.1E+1.2W 
1995 Sep 10    1436.20 35741 x 35835 x 1.6 GEO 79.7E 
1995 Sep 30    1436.07 35744 x 35827x 1.5 GEO 79.8E 
1996 Aug 1    1436.12 35761 x 35812 x 0.8 GEO 80.4E 
1999 Oct 17    1436.07 35775 x 35796 x 1.6 GEO 80.2E 

A Season of Opera : From Orpheus to Ariadne

 https://welib.org/md5/4e18b71406a1ab6220b5b0f208425d8e

Spaceflight: February 2001

 https://welib.org/md5/837b9fe82e62b209e5f3bd06512ce374

Progress M-38

 1998-015A


7K-TGM No. 240 was modified to carry a VDU. Launch mass was 7007 kg. After undocking Progress 240 made some test engine burns which were observed by the crew.


Progress M-38 
 

DateTimeEventOrbit  

1998 Mar 14  2245:55  Launch by Soyuz-U 
 2250  Blok-A sep 
 2250  Blok-I burn 
 2254:44  Blok-I sep 
1998 Mar 15  0227:54  TCM-1 
 0319:45  TCM-2 
1998 Mar 17   Kurs failure at 40m 
  TORU approach from 20m 
1998 Mar 17  0031:17  Docked with Kvant 
 0206  Hatch open 
1998 May 15  1841  Undocked 
 1914  Engine test burns 
 1951  last test burn 
1998 May 16  2155Deorbit 
 2220  Reentered 

Tuesday, February 6, 2001

Marco Polo 1

 1989-067A


British Satellite Broadcasting's BSB R1 satellite was named Marco Polo 1, after the Italian explorer Marco Polo (1254-1324), once it was launched in Aug 1989. In Dec 1993 the satellite was sold to Nordiska Satellitaktiebolaget (NSAB) of Sweden and renamed Sirius 1.


Marco Polo 1 (Sirius 1) 
 

DateTimeEventOrbit  

1989 Aug 27  2259  Launch by Delta 4925  LC17B 
  T+0:55 SRM 1-6 out 
  T+1:00 SRM 7-9 on 
  T+1:01 SRM 1-3 sep 
  T+1:02 SRM 4-6 sep 
  T+1:56 SRM 7-9 out 
  T+2:02 SRM 7-9 sep 
  T+4:24 MECO 
 2303 T+4:31 St 1 sep 
  T+4:37 SES-1 Stage 2 burn 127 km 
  T+4:41 Fairing 130 km 
 2310 T+11:32 SECO 188 km  180 x 330 x 28.5? (PK) 
 2320 T+21:52 SES-2 
 2320 T+21:57 SECO-2  181 x 438 x 26.7? (PK) 
 2321 T+22:50 Stage 2 sep  
 2322  T+23:27 Stage 3 burn 
 2323 T+24:54 TECO  203 x 36913 x 23.2 
 2325  T+26:47 Stage 3 sep 
 2325 T+26:49 Yo weight  
1989 Aug 28  0019 T+1:20:00 SES-3 depletion  
 0019 T+1:20:11 SECO-3  287 x 492 x 26.7  
1989 Aug 29  1352  AKM Star 30BP fired 
1989 Aug 31   Solar array deploy 
1989 Sep 1    1435.84 35778 x 35784 x 0.1 GEO 30.4W+0.05W 
1989 Sep 30    1436.28 35782 x 35798 x 0.1 GEO 31.2W 
1989 Oct 14    1436.12 35779 x 35795 x 0.1 GEO 31.0W 
1990 Nov 2    Owner becomes BSkyB 
1992 Oct 2    1436.13 35780 x 35793 x 0.0 GEO 31.0W 
1993 Nov 28    1436.14 35782 x 35792 x 0.0 GEO 31.0W 
1993 Dec 13   Sold to NSAB  GEO 31W 
  Renamed Sirius 
1993 Dec 31    1436.12 35781 x 35793 x 0.1 GEO 31.0W 
1994 Jan 6?   mv out 
1994 Jan 7    1433.66 35725 x 35752 x 0.0 GEO 29.5W+0.6E 
1994 Feb 23   mv in  1436.03 35778 x 35792 x 0.0 GEO 5.3E 
1997 Sep 11    1436.04 35778 x 35792 x 0.0 GEO 5.2E 
1999 Jun 16    1436.08 35778 x 35794 x 0.0 GEO 5.2E 
2000 Mar 27    1436.04 35776 x 35794 x 0.6 GEO 5.3E 

Saturday, February 3, 2001

Molniya 189

 1996-045A



Molniya-1T F94 
 

DateTimeEventOrbit  

1996 Aug 14  2220:59 Launch by 8K78M  PL LC43/3 
 2225 T+4:46 Blok A sep 
 2225  T+4:56 KhO sep 
 2229 T+8:46 Blok-I MECO 
 2229  T+8:50 Blok-I sep   
 2314  T+53:16 BOZ burn 
 2314 T+53:56 BOZ sep 
  ML burn 
 2317  T+56:46 ML MECO 
 2317  T+56:54 ML sep   
1996 Aug 20    736.05 457 x 40794 x 62.9 
1996 Aug 22   mv in  718.62 459 x 39936 x 62.8 
1996 Aug 26    717.79 464 x 39891 x 62.8

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...