proposed us contribution to the wide field imager psu mit jhu
TRANSCRIPT
History
• PSU, MIT, and SAO approached about four years ago to contribute to IXO WFI instrument.
• Proposed US contribution to IXO WFI was in the ICU hardware and software.– This provided a clean interface between US and European
hardware.– Drew upon decades of combined US experience with X-ray
imaging instruments• Murray/SAO-JHU: Einstein HRI, ROSAT HRI, Chandra HRC• Bautz/MIT: ASCA SIS, Chandra ACIS, Suzaku XIS, Astro-H SXI • Burrows/PSU: Chandra ACIS, Swift XRT
US Response to L2
• Paul Hertz (director of NASA’s Astrophysics Division) has expressed interest in contributing to an L2 mission at a level of up to $150M.
• The US X-Ray Science Interest Group (XRSIG) prepared a list of possible US contributions to ESA’s L2 mission for Paul’s consideration. This list included a US contribution to the ATHENA WFI instrument along the lines of the IXO contribution.
• ESA Call for L2 Mission Concept proposals clearly permits US contributions to Instrument Teams
• The current WFI architecture is similar to the IXO WFI architecture as of summer 2010
High speed fiber optic data link proposed
2048 x 2816 pixels total, read out every 2 μs (?) => 1 Gpix/s – 1.5 Gpix/s
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Proposed US contribution to WFI
US contribution
US contribution: ICU •Provides clean interface between US and European responsibilities•Capitalizes on initial development of high-speed event recognition•Propose fiber optic data transfer bus to WFI
Movable Instrument Platform
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Fiber Optic interface• Assumed 8 optical fibers (for IXO/WFI)
– Mass < 500 g– Power < 3W– Cost ~ $70K – Double numbers for redundancy
• Requires use of Xilinx FPGAs to interface to optical fiber transceivers– Xilinx Virtex-5QV FPGAs are rad-hard, 1 Mrad dose– Virtex-5 are fast enough, >3 GHz multi-gigabit serial
IXO WFI Instrument Control Unit Block Diagram June 2010 D. Burrows
Spacecraft Com
GSE connection
Power
Science Data
Housekeeping Data
Slow Control Bus
Housekeeping / Relays / Mechanisms
Instrument Processor Board(128K PROM, 512K EEPROM,4MB SRAM, 512MB SDRAM)
Frame Builder 1Custom FPGA / SRAM
Power Supply BoardS
pac
ec
raft
Comm / Mem Board(512 MB Flash)
S/C Power
Spacewire
ICU Block Diagram
Frame Builder 2Custom FPGA / SRAM
To Filter Wheel Stepper Motor
To APS Htr
+3.3V Digital Power
To HPP
(x2)+1.7V ASIC Power
ASIC Substrate Power
Fiber Optic Cables from HPPs
1 PPS
Slow Control
(Spacewire)
ICU Concept• 2.5mm Al chassis for shielding (5 kg)• 3U/6U box, 6 slot backplane (488 g)
– Slot 0: LVPS (500 g, 11.25 W @ 70%)– Slot 1: 3U System Slot, Instrument Processor Board (450 g, 3.55 W)
• Instrument control, telemetry formatting
– Slot 2: 6U Comm/Memory Board (880 g, 3.55 W)– Slot 3: 6U Frame Builder Board 1 (880 g, 6.25 W)– Slot 4: 6U Frame Builder Board 2 (880 g, 6.25 W)– Slot 5: 6U HK / Relay / Mechanism Board (880 g, 6.50 W)– Slot 6: spare
• Total mass: ~ 10.0 kg• Total power: 37.4 W
ICU Concept• Mass (IXO PDD allocation is 26.5 kg, w/
redundancy):– Total mass: 10.0 kg (CBE)– Total redundant mass: 25.9 kg (CBE+30%)
• Power:– ICU Power: 37.4 W (CBE)– Total + 20%: 44.9 W (CBE + 20%)
Summary
• PSU, MIT, and JHU are excited to have a chance to contribute to this mission!
• Interested in ICU:– Power, mechanism control– Frame builder and telemetry formatting– Hardware and software– Joint development by PSU, MIT, JHU
• Note that we also have experience in large thin filters for Chandra (HRC and ACIS)
Proposed US Contribution to WFI• Based on IXO WFI instrument teaming arrangements• Proposed US contribution: frame builder and event processing
software• PSU: provide high-speed digital framework, high-speed fiber interface to FEE • JHU: frame builder (event recognition)• MIT: flight software (event processing)
• Builds on decades of combined experience in X-ray imaging instruments, including • Murray/SAO-JHU: Einstein HRI, ROSAT HRI, Chandra HRC• Bautz/MIT: ASCA SIS, Chandra ACIS, Suzaku XIS, • Burrows/PSU: Chandra ACIS, Swift XRT
Fiber Optic interface to ICU
www.spacephotonics.com
Design flexibility, good radiation tolerance, high speed, low power
FEE
ADCADC
ADCADC
ADCADC
ADCADC
FPGAFPGA
FPGAFPGA
FPGAFPGA
FPGAFPGA
CAMERACAMERAFlex cableFlex cable Flex cableFlex cable
Instrument Control
CPUCPU
Frame Builder S/C I/FS/C I/F
Slow Control/ConfigSlow Control/Config
Power Conditioning
H/KH/K
Image Controller / APS Sequencer
Image Controller / APS Sequencer
Controller Power
Controller Power
Heater Power/Con
trol
Heater Power/Con
trol
ASIC PowerASIC Power
Sensor PowerSensor Power
Processor Power
Processor Power
JHUJHU
PSUPSU
ULUL
MITMIT
mechanism controls
mechanism controls
SoftwareSoftware
WFI baseline
ICU
WFI ICU1) CPU = Brain + Slow control2) PSB: low voltage power supplies3) S/C Interface (SpaceWire?)4) Camera Interface (serial optical + SpaceWire?)5) HK: all HK from outside the ICU will be digitized
locally and provided to ICU on the slow control bus6) Heater power / mechanisms
1) Detector temperature control2) Filter stepper motor (if needed)3) any other heaters or mechanisms
7) Frame Builder (JHU)1) Frame buffer2) Event recognition and formatter
8) System Software (PSU/SwRI)1) O/S, drivers, S/C interface, heater control, ...
9) Science Software (MIT/JHU)
+ Fully Redundant B-side
1) CPU = Brain + Slow control2) PSB: low voltage power supplies3) S/C Interface (SpaceWire?)4) Camera Interface (serial optical + SpaceWire?)5) HK: all HK from outside the ICU will be digitized
locally and provided to ICU on the slow control bus6) Heater power / mechanisms
1) Detector temperature control2) Filter stepper motor (if needed)3) any other heaters or mechanisms
7) Frame Builder (JHU)1) Frame buffer2) Event recognition and formatter
8) System Software (PSU/SwRI)1) O/S, drivers, S/C interface, heater control, ...
9) Science Software (MIT/JHU)
+ Fully Redundant B-side