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NASA Hubble Space Telescope Daily Report # 3802

 
STATUS REPORT
Date Released: Tuesday, February 22, 2005
Source: Space Telescope Science Institute


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DAILY REPORT        # 3802

PERIOD COVERED: DOY 52

OBSERVATIONS SCHEDULED

ACS/WFC/HRC/NIC2 10443

ACS & WFPC2 Two-gyro PSF, pointing and dither test

12 orbits High priority observations {5 orbits} will be observed together at start of two- gyro SMS as contingency against HST failure. Remaining 7 orbits provide further tests and additional experience in two-gyro mode. It is believed that this will be the only test prior to final failure into two-gyro mode. Goals: PSF, PSF repeatability, pointing and stability within the orbit {requirements 1a, 1c, 2 , 4}

FGS 10457

2-Gyro F2G Test Miscellaneous Orbits

This proposal is part of the February on-orbit 2-gyro testing.

NIC1/NIC2 10447

NICMOS Dither Test two-gyro mode

The accuracy of the combined dither and chop mode in NICMOS running in two-gyro mode is tested. Dithering permits the removal of dead or non-calibrated pixels on the detectors and improves the spatial sampling and the effects of detector non- uniformities. Chopping is used for mapping and background subtraction. The latter can involve large offsets in order to find blank sky. In this test we use the NIC-SPIRAL- DITH-CHOP pattern with a dither step of 1.5" and a chop of 100". The chop distance is small enough that a re-acquisition of the guide star is not required {chosen before larger chop distance because of time constraint}. NIC1 and NIC2 cameras are involved, where NIC2 is primary and NIC1 parallel.

NIC1/NIC2/NIC3 10446

NICMOS 2Gyro PSF-test

This proposal is aimed at analyzing the NICMOS PSF under 2-gyro operations. For that we will observe the standard star P330E, which has been intensively observed since Cyle 7 and, therefore, it is a good reference to detect any possible deviation from 3- gyro operations. This proposal is largely based on the photometric monitoring calibration proposal {10381 and previous}. Changes with respect to that proposal include: 1- The patterns are repeated twice for NIC1, and 3 times for NIC2 in order to gain S/N and reduce intrapixel sensitivity. NIC3 observations {1 repeat} complete the last orbit. 2- For F110W observations the SCAMRR sequence is used instead of MCAMRR, in order to gain temporal resolution. 3- Filters F190N and F222M will not be observed with NIC3. The effects of jitter on these filters should be very small {and better detected with NIC2}. Intrapixel sensitivity variations induced by the jitter should be better studied at shorter wavelengths.

NIC1/NIC2/NIC3 8792

NICMOS Post-SAA calibration - CR Persistence Part 3

A new procedure proposed to alleviate the CR-persistence problem of NICMOS. Dark frames will be obtained immediately upon exiting the SAA contour 23, and every time a NICMOS exposure is scheduled within 50 minutes of coming out of the SAA. The darks will be obtained in parallel in all three NICMOS Cameras. The POST-SAA darks will be non-standard reference files available to users with a USEAFTER date/time mark. The keyword 'USEAFTER=date/time' will also be added to the header of each POST-SAA DARK frame. The keyword must be populated with the time, in addition to the date, because HST crosses the SAA ~8 times per day so each POST-SAA DARK will need to have the appropriate time specified, for users to identify the ones they need. Both the raw and processed images will be archived as POST-SAA DARKSs. Generally we expect that all NICMOS science/calibration observations started within 50 minutes of leaving an SAA will need such maps to remove the CR persistence from the science images. Each observation will need its own CRMAP, as different SAA passages leave different imprints on the NICMOS detectors.

NIC2 10448

NICMOS 2-gyro Coronagraphic Performance Assessment

Coronagraphic acquisition should not be affected by transitioning from 3-gyro to 2-gyro mode guiding. However, coronagraphic performance is dependent upon positioning of a target within the coronagraphic hole and the ability to obtain a second observation with a roll of the telescope within the same visibility period. Observations of a bright target are needed to verify and confirm the coronagraphic performance, the ability to suppress the diffractive energy background and the stability to image coronagraphically occulted targets at two field orientations {rolls}.

FLIGHT OPERATIONS SUMMARY:

Significant Spacecraft Anomalies: (The following are preliminary reports of potential non-nominal performance that will be investigated.)

HSTAR 9714 : GSacq(1,3,1) failed to RGA Control @ 052/1331z - The GSAcq(1,3,1) scheduled at 052/13:31:32 achived F2G-FL, then transitioned to RGA control (1.e) F2G-FL/T2G/M2G Mode. Stop flag indication was observed. Prior OBAD at 052/13:11:45, and 052/13:23:12 were successful.  Possible Observations affected:  NIC 11 thru 16.   Under investigation.

HSTAR 9716 : GSAcq(1,3,1) failed to RGA control during F2G On-Orbit Test @ 052/1507z - The GSAcq(1,3,1) scheduled at 052/15:07:32 during F2G On-Orbit Test achived F2F-FL, then failed to RGA control (i.e)   transitioned to F2G/T2G Mode. Stop indication flag was observed. Same guide star id per ref HSTAR 9714.  Prior OBAD at 052/14:47:42, and 052/14:59:12 were successful.Possible Observations affected: NIC 17 thru 22. Under investigation.

COMPLETED OPS REQs: 17370-0 - Continuous Engineering Coverage for F2G OOT (ESTR2 Power ON) @ 052/1440z

17370-0 - Continuous Engineering Coverage for F2G OOT (ESTR2 Record to 18.41%)                 @ 052/1440z-1535z

17383-0 - Patch Acq. Logic for Target ReAcq @ 053/0017z

17370-0 - Continuous Engineering Coverage for F2G OOT (ESTR2 Record  to 34.74%)                 @ 053/0117z-0210z

17370-0 - Continuous Engineering Coverage for F2G OOT (ESTR2 to BOT) @ 053/0528z

OPS NOTES EXECUTED: None

                              SCHEDULED     SUCCESSFUL    FAILURE TIMES 
 FGS Gsacq                   7                         7 
 FGS 
 Reacq                   7                         5               052/1331z 
 (HSTAR 9714) & 
                                                                                  052/1507z 
 (HSTAR 9716) 
 FHST Update 
 OBAD                           28                      28 
 LOSS of LOCK 

SIGNIFICANT EVENTS:

The 3-day Two-Gyro Science (TGS) on-orbit test is in progress.

This test was the first use of a STScI generated TGS science mission timeline (SMS). HST was commanded into Two-Gyro Mode on Feb 20th at ~8:00 pm EST.  The new Fine Guiding Mode (F2G) mode is performing well, and HST boresight jitter is similar to PCS predictions.


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