Wednesday, April 26, 2000

Aviation Week: October 4,1999

 https://welib.org/md5/23e54b80fe75e242ca3cadfe03224d91

Vortex 11

 1984-009A


A rumour that VORTEX 11 had a Transtage failure and was stranded in transfer orbit was probably incorrect and arose from the DoD's practice of only announcing the transfer and not the final orbit.


VORTEX 11 
 

DateTimeEventOrbit  

1984 Jan 31  0308:00  Launch by Titan 34D/Transtage  CC 
  T+1:50 Stage 1 ignition 
  T+2:02 SRM sep 
  T+4:35 St 1 sep 
 0312 T+4:45 Fairing sep 
 0316  Stage 2 MECO 
 0316 T+8:05 Stage 2 sep 
 
 0330?  Transtage burn 1 (310s) 
 0335?  Burn 1 cutoff 
  5h15m coast 
 0850?  Transtage burn 2 (110s) 
 0852? Burn 2 cutoff 
 0900? Transtage sep 
1984 Feb 1   (r/b) 96.3 145 x 1022 x 29.3 
1984 Feb 10?    1436.0 31200 x 40200 x 5.0

Tuesday, April 25, 2000

Kosmos 1870

 1987-064A


Almaz earth observation platform, 4.1 dia x 7 l. 2.5 kW solar power, 4 tonne payload. Kosmos-1870 was Mech-K No. 304 and was the Soviet Union's first radar imager.


Kosmos-1870 
 

DateTimeEventOrbit  

1987 Jul 25  0900:00 Launch by Proton  KB 
  Stage 1 sep (T+2:06) 
  Stage 2 sep (T+5:34) 
  Stage 3 MECO (T+9:30) 
 0909:44 Stage 3 sep (T+9:44)  
1987 Jul 25.5   88.40 160x231x71.94 
1987 Jul 25.7   88.65 159x256x71.9 
1987 Jul 28.5    89.36 237x249x71.9 from 88.54 157x247 
1987 Jul 29.3   89.55 245x260x71.9 
1987 Aug 10    89.58 252x256x71.9 from 89.48 241x256 
1987 Aug 22    89.55 247x258x71.9 from 89.50 247x252 
1987 Sep 3    89.58 242x265x71.9 from 89.45 242x253 
1987 Sep 15    89.56 244x262x71.9 from 89.49 238x261 
1987 Sep 26    89.57 241x265x71.9 from 89.47 240x257 
1987 Nov 1    89.58 239x269x71.9 from 89.42 238x253 
1987 Nov 13    89.58 245x262x71.9 from 89.45 232x263 
1987 Nov 26    89.58 246x262x71.9 from 89.45 240x256 
1987 Dec 8    89.57 251x256x71.9 
1987 Dec 18    89.55 245x259x71.9 from 89.48 246x251 
1987 Dec 30    89.58 242x266x71.9 from 89.46 242x254 
1988 Jan 11   89.59 247x261x71.9 from 89.47 237x260 
1988 Jan 23    89.58 239x269x71.9 from 89.46 242x254 
1988 Feb 4    89.55 244x260x71.9 from 89.47 237x260 
1988 Feb 14    89.44 235x250x71.9 
1988 Feb 16    89.60 245x264x71.9 from 89.42 238x254 
1988 Feb 28    89.57 249x258x71.9 from 240x258 
1988 Mar 10    243x265x71.9 from 243x257 
1988 Mar 22    249x260x71.9 from 238x260 
1988 Apr 4    89.59 241x268x71.9 
1988 Apr 15    89.59 246x263x71.9 from 234x260 
1988 Apr 27    254x255x71.9 from 240x255 
1988 May 9    89.58 245x263x71.9 from 247x249 
1988 May 21    89.59 253x255x71.9 from 89.45 239x256 
1988 Jun 2    89.56 246x261x71.9 from 89.45 246x249 
1988 Jun 14    89.59 246x263x71.9 from ? 
1988 Jun 25    89.66 253x262x71.9 from 89.46 238x257 
1988 Jul 6    89.60 244x265x71.9 from 89.43 240x253 
1988 Jul 19    89.58 249x259x71.9 from 89.47 237x259 
1988 Jul 31    89.58 244x264x71.9 from 89.45 242x253 
1988 Aug 12    89.60 250x260x71.9 from 89.44 237x256 
1988 Aug 24    89.60 244x266x71.9 from 89.45 242x253 
1988 Sep 5    89.60 252x258x71.9 from 89.41 234x259 
1988 Sep 17    89.90 262x277x71.9 from 89.43 245x248 
1988 Oct 11    89.96 264x281x71.9 from ? 
1988 Nov 3    89.90 263x277x71.9 from 89.61 248x262 via 89.73 259x264 
1988 Nov 27    89.94 264x279x71.9 from 89.53 245x258 
1988 Dec 21    89.91 263x277x71.9 from 89.60 249x261 
1989 Jan 13    89.96 265x280x71.9 from 89.50 244x255 
1989 Feb 6    89.98 267x280x71.9 from 89.53 246x257 
1989 Mar 3    89.93 266x280x71.9 from 89.51 244x252 
1989 Mar 27    90.00 267x282x71.9 from 89.48 243x255 
1989 Apr 20    89.98 266x281x71.9 from 89.52 244x258 
1989 May 13    89.91 264x276x71.9 from 89.56 246x260 
1989 Jun 7    89.94 265x278x71.9 from 89.48 242x256 
1989 Jul 1    89.99 266x281x71.9 from 89.49 241x257 
1989 Jul 24    89.58 242x264x71.9 from 89.67 251x265 

Monday, April 24, 2000

TOMS-EP

 1996-037A


The TOMS-Earth Probe, TOMS-EP94, carried a single experiment, Total Ozone Mapping Spectrometer Flight Model 3. TOMS FM1 had flown on Nimbus 7, and FM2 flew on a 1991 Meteor satellite. TOMS-EP, originally Earth Probe '93, had been intended for launch in 1993 to take over from TOMS FM2, which eventually failed in 1994. The problems with the Pegasus launch vehicle delayed it to 1996, placing it close to the planned launch of FM4 on Japan's ADEOS. Its mission was altered to lower the target orbit from the original 900 km to 500 km for higher resolution studies.

The TOMS instrument was derived from the older SBUV first flown on Nimbus 4 in 1970. Mission operations from GSFC.

In Jul 1996 it was finally launched on the fourth Pegasus XL, carried aloft by the L-1011 carrier plane from Vandenberg. The three stage Pegasus delivered it to an elliptical polar orbit.

A monopropellant hydrazine propulsion engine delivered TOMS-EP to its final circular orbit. TOMS used TRW's STEP/Eagle class T-200 Lightsat bus, based on Defense Systems (DSI) technology. Launch mass of TOMS-EP was 295 kg including 73 kg of propellant. The satellite is 1.8m long x 1.1m wide; with solar arrays deployed 2.4 x 3.9m.


TOMS-EP94 
 

DateTimeEventOrbit  

1996 Jul 2   L-1011 takeoff from Vandenberg 
 0748  T-0:05 Pegasus drop at 38kft, launch  
  T+0:00, D+0:05 Stage 1 burn 
  T+1:15 Stage 1 burnout 
  T+1:32 Stage 1 sep, stage 2 burn 
  D+2:27 Fairing  
 0750 D+2:41 Stage 2 burnout 
 0753 D+5:58 Pegasus stage 3 burn 
 0754? Stage 3 burnout 
 0756  D+8:07? Pegasus stage 3 sep  345 x 953 x 97.4 (OSC) 
1996 Jul 3    340 x 943 x 97.4 
1996 Jul 5    97.56 340 x 943 x 97.4 
1996 Jul 8   Orbit raise 
1996 Jul 11    94.67 494 x 511 x 97.4 
1996 Jul 25    94.66 494 x 510 x 97.4 
1996 Aug 23    94.67 492 x 512 x 97.4 
1997 Mar 15    94.61 489 x 509 x 97.4 
1997 Dec 4    94.51 486 x 503 x 97.4 
1997 Dec 6   orbit raise  94.96 498 x 535 x 97.57 
1997 Dec 7   orbit raise  95.51 497 x 588 x 97.87 
1997 Dec 8   Orbit raise to replace ADEOS  96.47 582 x 596 x 97.9 
1997 Dec 15   orbit raise  99.65 737 x 746 x 98.4 
1998 Jan 28    99.65 737 x 746 x 98.4 

May 13,2026

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