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Chandra X-Ray Observatory CXC Paul Plucinsky EPI Cal 2010 1 Update on ACIS Operations I.New Patch for ACIS Flight SW II.Control of the ACIS FP temperature
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Chandra X-Ray Observatory CXC Paul Plucinsky EPI Cal 2010 2 Update to the ACIS Flight SW ACIS flight SW has been updated three times during the mission in 2000, 2004, & 2008 We are preparing the fourth patch for uplink in Spring 2010 This new patch contains two new items: 1)Fixes a bug in a subarray mode – the list of bad pixels and columns onboard is misinterpreted if the subarray starts in a row other than row 1 2)Prevents Back End Processor (BEP) from crashing when one of the Front End Processors (FEPs) is powered down - there have been several occurrences when radiation levels have been high, that ACIS was commanded by the stored command load to start the first science observation of the orbit, it started collecting the bias data, but then received a high radiation shutdown signal from the satellite, but ACIS waits for the bias maps to be collected before stopping the science run, but before the bias maps are collected a command is sent which powers down the FEPs, this caused the BEP to crash in the past
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Chandra X-Ray Observatory CXC Paul Plucinsky EPI Cal 2010 3 Control of the ACIS FP Temperature Desired temperature -119.7 C, FI/BI CCDs go out of gain spec at -119.2C/-118.2 C Mean T of science observations ACIS DH heater turned off in April 2008 SIM FA6 heater turned off in August 2009
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Chandra X-Ray Observatory CXC Paul Plucinsky EPI Cal 2010 4 Controlling the ACIS FP Temperature FP is contained in the “Camera Body” DH heater is on the “Camera Body” Camera Body used to be held at -60 C, it now floats between -65 and -70 C
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Chandra X-Ray Observatory CXC Paul Plucinsky EPI Cal 2010 5 Exploded View of ACIS HW
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Chandra X-Ray Observatory CXC Paul Plucinsky EPI Cal 2010 6 Restrictions on Spacecraft Attitude unfortunately there are no other heaters we can turn off which would help to keep the FP cold must now consider imposing restrictions on the satellite’s orientation during observations (which is already done for several other systems on Chandra)
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Chandra X-Ray Observatory CXC Paul Plucinsky EPI Cal 2010 7 Impact of Current Restrictions on Spacecraft Pitch Angle restrictions imposed in 2005 significantly increased the amount of time spent at tail-Sun attitudes, pitch>115 unfortunately this is a hot attitude for the ACIS FP temperature
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Chandra X-Ray Observatory CXC Paul Plucinsky EPI Cal 2010 8 Chandra in the Shuttle Bay Before Launch thermal properties of the back surfaces of SIM are changing with time
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Chandra X-Ray Observatory CXC Paul Plucinsky EPI Cal 2010 9 Chandra in the Shuttle Bay Before Launch heating on the back surface of the SIM, heats the ACIS Camera Body heating of the shade for the radiator, heats the radiator
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Chandra X-Ray Observatory CXC Paul Plucinsky EPI Cal 2010 10 Earth in the ACIS Radiator FOV Earth in the ACIS radiator FOV has a significant impact on the FP temperature The complex shape of the shade has been approximated by a simpler shape, we are working on a more realistic model we recently included reflections off of the interior surfaces of the shades
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Chandra X-Ray Observatory CXC Paul Plucinsky EPI Cal 2010 11 ACIS FP Temperature vs. Earth Solid Angle Without Reflections Adams -Wolk (SAO)
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Chandra X-Ray Observatory CXC Paul Plucinsky EPI Cal 2010 12 ACIS FP Temperature vs. Earth Solid Angle With Reflections Adams -Wolk (SAO)
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Chandra X-Ray Observatory CXC Paul Plucinsky EPI Cal 2010 13 Future Strategies to Keep the ACIS FP Cold 1) Earth in the ACIS radiator FOV 2) Sun on the back surfaces of the SIM and the radiator shade There are two reasons the ACIS FP temperature gets warm now: Our only option now is to impose restrictions on the spacecraft attitude, but that will be difficult because:
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Chandra X-Ray Observatory CXC Paul Plucinsky EPI Cal 2010 14 Backup Material
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Chandra X-Ray Observatory CXC Paul Plucinsky EPI Cal 2010 15 Chandra’s Changing Orbit and Implications for the FP Temperature Chandra’s orbit is changing such that in 2012 the inclination will be at its highest value in the mission and the perigee will be at it lowest the solid angle of the Earth in the ACIS radiator FOV will also reach missions highs in 2012 other mission constraints such as momentum management and thermal issues frequently conflict with keeping the ACIS FP cold during perigee passages Davis (Chandra FOT )
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Chandra X-Ray Observatory CXC Paul Plucinsky EPI Cal 2010 16 The FP Temperature during Recent Perigee Passages science cal perigee Example of a good perigee passage Adams-Wolk (SAO )
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Chandra X-Ray Observatory CXC Paul Plucinsky EPI Cal 2010 17 The FP Temperature during Recent Perigee Passages science cal perigee Example of a bad perigee passage Adams-Wolk (SAO )
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