Tuesday, February 12, 2019

Rossi X-Ray Timing Explorer

 1995-074A


The Bruno B. Rossi X-Ray Timing Explorer (RXTE) was intended for studies of the time variability and spectra of bright X-ray sources in the hard X-ray (2 keV and above). Known before Mar 1996 as simply XTE, the satellite used a bus built at NASA-Goddard with steerable solar arrays, reaction wheels, and high gain TDRS antennae to allow all-sky access and rapid maneuvrability. The bus was 5.8 x 1.8 x 1.8m in size. It could point to 6 arcmin with a 10 degree per minute slew rate; mass of XTE was 2955 kg. XTE was named after Bruno Rossi (1905-1993), a former MIT physicist who was one of the founders of X-ray astronomy.

Launch was postponed many times because of the Koreasat launch problem and because of weather delays. The first ignition attempt on Dec 22 was aborted when a frozen LOX valve prevented main engine ignition. Launch finally came on 1995 Dec 30.

The satellite was retired in 2012 after a successful career.


RXTE 
 

DateTimeEventOrbit  

1995 Dec 30  1348:00  Launch by Delta 7920-10 (Delta230)  CC LC17A 
 1347:57  Verniers ignite (T-3s) 
 1347:57  Main engine ignition (T-2.5s) 
 1348:00  GEM 1,2,3,7,8,9 ignite (T-0.25s) 
 1348:00  Liftoff 
 1349:03  GEM 1-3,7-9 burnout (T+1:03) 
 1349:05  GEM 4-6 ignite (T+1:05) 
 1349:06  GEM 1-3,7-9 sep (T+1:06) 
 1350:08  GEM 4-6 burnout (T+2:08) 
 1350:11  GEM 4-6 sep (T+2:11), 60 km 
 1352:20  RS-27 MECO (4:20), 133 km 
 1352:29  Thor sep (4:29) 
 1352:34  Delta ignition (4:34), 140 km 
 1352:40  Fairing (10-foot) sep (T+4:40), alt 143 km 
 1357:55  Delta SECO1 (T+9:55), 181 km  157 x 613 x 28.73 
 1456:18  Delta burn 2 (T+1:08:18 for 1:31) 
 1457:49  Delta SECO2 (T+1:09:49) 
 1506:25  Delta sep from XTE (T+1:18:25)  565 x 583 x 23.0  
 1507:07 Delta retro cutoff (T+1:19:07) 
 1526:45 Delta evasive burn (T+1:38:45)  
 1526:50 Delta SECO 3 (T+1:38:50) 
 1534:40  Delta depletion burn (T+1:46:40) 
 1536  Delta SECO 4 command  176 x 575 x 25.0 (Delta) 
2012 Jan 4   Last science data 
2012 Jan 5   Decommissioned 
2018 Apr 30   Reentered 

Payload:

  • PCA Proportional Counter Array 5 Xe pc's 6250cm2 2-60 keV 1 deg FOV, 1 mus

  • HEXTE High Energy X-ray Timing Experiment1600 cm2 20-200 keV 1 deg FOV, 10 mus

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