Friday, September 29, 2000

Compton Gamma Ray Observatory

 1991-027B


Known simply as GRO (Gamma Ray Observatory) before launch, this spacecraft was renamed the Arthur Holly Compton Gamma Ray Observatory, CGRO, in honor of the American physicist (1892-1962) after whom the Compton Effect of gamma-ray/electron interactions is also named. The spacecraft was built by TRW and operated by GSFC.

CGRO was deployed by Atlantis' RMS arm at 2235 on 1991 Apr 7 into a 93.63 min, 446 x 458 km x 28.5 deg orbit. The most dramatic early results from CGRO were the discovery by EGRET of the gamma-ray loud quasars, and the results from BATSE indicating that gamma ray burst sources were distributed uniformly across the sky.

CGRO had an internal propulsion system to raise its orbit. The GRO propulsion system, built by TRW, had a mass of 281 kg dry and 1920 kg of monopropellant hydrazine, with four thruster modules each with two MRE-5 thrusters. The OAT (Orbit Adjust Thrusters) had some initial pressurization problems just after launch, so it was decided to use a smaller set of thrusters for the orbit adjust. A test firing was carried out on 1993 May 4, and the B-side thrusters were fired twice on 1993 Jun 15, but the second time one thruster did not fire and the burn was aborted. It was decided to go back to using the OATs. Test burns were made on Aug 3, Aug 17 and Sep 7. The first true orbit raising burn was made on Oct 4 around 0500; 6 more burns were made between Oct 6 and 1828 on Oct 14. By Oct 12 the orbit had been raised back to 341 x 446 km x 28.5 deg.

Tape recorder failures limited the amount of data CGRO could send back, so in 1994 the TDRS 1 satellite was moved over a new ground station in Tidbinbilla, Australia to improve data coverage.


GRO 
 

DateTimeEventOrbit  

1991 Apr 8    93.63 446 x 458 x 28.5 
1992 Dec 1    92.06 372 x 378 x 28.5 
1993 Feb 26    91.77 357 x 364 x 28.5 
1993 May 1    91.47 344 x 348 x 28.5 
1993 May 13    91.55 348 x 352 x 28.5 
1993 May 25    91.52 347 x 351 x 28.5 
1993 Jun 10    91.46 344 x 347 x 28.5 
1993 Jun 21    91.56 347 x 354 x 28.5 
1993 Aug 3    91.45 341 x 350 x 28.5 
1993 Aug 12    91.43 340 x 348 x 28.5 
1993 Aug 18    91.42 338 x 349 x 28.5 
1993 Sep 1    91.38 336 x 347 x 28.5 
1993 Sep 8    91.37 336 x 346 x 28.5 
1993 Oct 2    91.29 333 x 342 x 28.5 
1993 Oct 9    91.66 340 x 371 x 28.5 
1993 Oct 14    345 x 409 x 28.4 
1993 Oct 21    92.44 341 x 446 x 28.5 
1997 Mar 24   ACT engineering test burn  
1997 Mar 26   OAT engineering test burn  
1997 Apr 1  1800 OAT 90s reboost  
1997 Apr 2  1900 OAT 90s reboost 
1997 Apr 3  1830 OAT 90s reboost 
1997 Apr 5  1900 OAT 90s reboost 
1997 Apr 6  1700 OAT 90s reboost   
2000 May 10    94.31 482 x 487 x 28.5 
2000 May 31  0151  Descent burn 1 23:06 92.94 362 x 474 x 28.5  
2000 Jun 1  0236 Burn 2, 26min  91.62 237 x 471 x 28.5  
2000 Jun 4  0356 Burn 3, 21:39   
 0417  Burn 3 cutoff  146 x  

0522:21 Burn 4, 30 min, 36.8 m/s 
 0552  Burn 4 cutoff  27 x  
 0609  Tumble maneuver
 0610  loss of contact 
 0613  Reentry at 50 km 
 0618  Impact in Pacific SE of Hawaii 

Payload:

  • OAT Orbit Adjust Thrusters; 4 Rocket Research Corp 445N thrusters, 8 TRW MRE-5 22N thrusters.

  • BATSE The Burst and Transient Source Experiment, a NASA-MSFC experiment to detect, locate, and measure the light curves and spectra of gamma ray bursts; 20 keV - 1 MeV

  • EGRET The Extreme Gamma ray Event Telescope, to detect gamma ray sources in the 100 MeV range. (20 MeV-30 GeV)

  • COMPTEL Imaging Compton Telescope 1-30 MeV

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