Tuesday, June 22, 2004

International Ultraviolet Explorer

 1978-012A


The International Ultraviolet Explorer was designed for a six month mission but was still operating 16 years later. IUE took ultraviolet spectra of astronomical objects - tens of thousands of them. It was the first astronomy satellite to be operated as an observatory, available for use by the whole astronomical community. Uniquely, it was in geosynchronous orbit, so that astronomers at the NASA-Goddard or ESA-Villafranca control centers could control the spectrographs in real time. IUE was jointly funded by NASA, ESA, and the UK Science Research Council; the orbit drifted back and forward across the Atlantic and observing was handled from the ESA ground station for 8 hours a day and from Goddard for 16 hours a day.

IUE was launched on 1978 Jan 26 at 1736 by a Delta 2914 from Cape Canaveral's Launch Complex 17A. The Delta stage entered a 96.6 min, 164 x 1024 km x 28.7 deg and separated from the third stage. The Star 37E third stage fired and placed IUE in a 846.7 min, 177 x 46367 km x 28.7 deg orbit. The Star 24 apogee motor fired to put the satellite in a final orbit of 1435.7 min, 25669 x 45888 km x 28.6 deg. Observations began a few days later. The internal propulsion system was used occasionally to maintain the satellite at the correct longitude.

On 1995 Oct 1 operational control of IUE was transferred completely to ESA-Villafranca. ESA and PPARC (the successor to SERC) would operate the spacecraft. IUE was shut down at 1842 UT on 1996 Sep 30.


IUE 
 

DateTimeEventOrbit  

1978 Jan 26  1736:00  Launch by Delta 2914  CC LC17A 
 0135:38  SRM 1-6 cutoff 
 0135:39  SRM7-9 burn 
 0136:17  SRM7-9 cutoff 
 0136:27  SRM 1-9 sep 
  T+3:42 MECO 
  T+3:49 Stage 1 sep 
  T+3:55 Stage 2 burn 
 1740 T+4:33 Fairing sep 
 1745 T+8:47 SECO-1 164 km vrel 7.807  167 x 167? x 28.7 
 1816 T+40:12 SES-2 172 km vrel 7.797  
 1816 T+40:30 SECO-2 172 km 8.024  96.6 164 x 1024 x 28.7 
 1817 T+41:22 Stage 2 sep 170 km 8.026 
 1818 T+42:03 TES 172 km 8.025 
 1818 T+42:47 TECO 176 km  846.7 177 x 46367 x 28.7 
 1819 T+43:50 S/C sep 204 km 
1978 Jan 27  0300? Apo 1 
1978 Jan 27  1454  Star 24 burn, apo 2  1435.7 25669 x 45888 x 28.6 
1978 Jan 28   Despin using HAPS 
1978 Jan 28  0602   1435.64 25668 x 45886 x 28.6 55.2W 
1978 Jan 30  1630  Dust cover ejected 
1978 Feb 1   First images from FES 
1978 Feb 9   First data currently in archive 
1978 Feb 13   Orbit correction 
1978 Mar 30    1436.38 25711 x 45872 x 28.6 51.8W 
1978 Jul 24   Orbit correction 
1979 Jun 20   Orbit correction 
1980 Feb 13   Orbit correction 
1980 Apr 18    1435.66 25888 x 45667 x 28.2 
1980 Jun 24   Orbit correction 
1980 Dec 16   Orbit correction 
1981 May 8   Orbit correction  1436.07 26080 x 45491 x 28.3  
1981 Oct 29   Orbit correction 
1982 Aug 17   Orbit correction 1435.54 26426 x 45125 x 28.6  
1983 May 27   Orbit correction 
1984 Jan 12   Orbit correction 
1984 Feb 14   Orbit correction 
1984 Nov 16   Orbit correction 
1985 Jul 16    1436.63 27451 x 44142 x 29.7 
1985 Aug 9   Orbit correction 
1985 Sep 6    1435.59 27533 x 44020 x 29.8 
1986 Mar 19   Orbit correction 
1986 Jul 29   Orbit correction  1435.81 27952 x 43609 x 30.2 
1986 Dec 18   Orbit correction 
1987 Sep 9  Orbit correction 
1988 Mar 18   Orbit correction 
1988 Sep 8   Orbit correction 
1989 Mar 13  Orbit correction 
1989 Sep 8  Orbit correction 
1990 Jun 6  Orbit correction 
1990 Dec 3    1436.35 29787 x 41795 x 32.6 53.5W 
1991 Jan 14    1436.46 29799 x 41787 x 32.3 56.9W 
1991 Jan 12   Orbit correction 
1991 Feb 6    1435.64 29811 x 41743 x 32.7 
1991 Nov 5    1436.74 29881 x 41716 x 33.0 57.4W 
1991 Oct 18   Orbit correction  1435.91 30045 x 41520 x 33.3 51.7W 
1992 Aug 18    1436.86 30160 x 41443 x 33.5 68.6W 
1992 Aug 19   Orbit correction  1435.72 30162 x 41395 x 33.5 68.0W 
1992 Nov 19    1436.07 30208 x 41363 x 33.7 64.3W 
1992 Nov 20   Orbit correction  1435.41 30213 x 41333 x 33.7 64.1W 
1993 Aug 17    1436.53 30264 x 41325 x 34.1 45.2W 
1993 Aug 19   Orbit correction  1435.77 30256 x 41304 x 34.1 46.1W 
1993 Sep 20    1435.84 30264 x 41299 x 34.2 51.1W 
1994 Feb 14    1436.49 30242 x 41346 x 34.5 57.4W 
1994 Feb 15   Orbit correction  1435.67 30243 x 41312 x 34.5 57.4W 
1994 Sep 20    1436.60 30235 x 41357 x 34.8 55.4W 
1994 Sep 20   Orbit correction  1435.55 30243 x 41308 x 34.8 52.9W 
1995 Apr 30    1436.58 30207 x 41384 x 35.1 48.4W 
1995 May 3   Orbit correction  1435.85 30183 x 41380 x 35.1 48.1W 
1995 Jun 5    1435.98 30178 x 41389 x 35.2 
1995 Jun 6   Orbit correction  1435.19 30162 x 41374 x 35.2 
1996 Mar 5    1436.21 30095 x 41482 x 35.6 35.8W 
1996 Mar 6   Command error, control lost 
1996 Mar 11   One-gyro control enabled 
1996 Sep 29    1437.04 29992 x 41617 x 35.9 65.5W 
1996 Sep 30  1357  Science cameras off 
 1730  Propellant drained (18 kg) 
 1842  Spacecraft deactivated 
1996 Oct 10    1439.04 30216 x 41472 x 35.6 
1999 Apr 27    1438.85 29739 x 41941 x 37.2 

Payload:

  • Telescope 45 cm Ritchey-Chretien telescope

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