SKARAB2 AUGUST 2017 Francois Kapp (and the DBE team, particularly - - PowerPoint PPT Presentation

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SKARAB2 AUGUST 2017 Francois Kapp (and the DBE team, particularly - - PowerPoint PPT Presentation

SKARAB2 AUGUST 2017 Francois Kapp (and the DBE team, particularly Adam and Jason) (also using a few SKAO slides) www.ska.ac.za SKA Key Science Drivers: The history of the Universe Cosmic Dawn T esting General Relativity (First Stars


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SLIDE 1

AUGUST 2017 Francois Kapp (and the DBE team, particularly Adam and Jason) (also using a few SKAO slides)

SKARAB2

www.ska.ac.za

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SLIDE 2

SKA– Key Science Drivers: The history of the Universe

Cosmic Dawn (First Stars and Galaxies) Galaxy Evolution (Normal Galaxies z~2-3) Cosmology (Dark Energy, Large Scale Structure) Cosmic Magnetism (Origin, Evolution) Cradle of Life (Planets, Molecules, SETI) T esting General Relativity (Strong Regime, Gravitational Waves) Exploration of the Unknown

Broadest range of science of any facility, worldwide

Image and text by SKA Organisati

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SLIDE 3

www.ska.ac.z a

Overview

Square Kilometre Array

  • 3 sites: 2 telescopes + HQ = 1 Observatory
  • Now in design Phase: ~ €200M; 600 scientists + engineers
  • Phase 1
  • Construction: 2019 – 2024
  • Construction cost cap: €674.1M (infmation-adjusted)
  • Operations planning now underway
  • MeerKat integrated
  • Observatory Development Programme
  • SKA Regional centres (locally funded)
  • Phase 2: start mid-2020s
  • Advanced Instrumentation Program to mature relevant technologies now
  • ~2000 dishes across 3500km of Southern Africa
  • Major expansion of SKA1-Low across Western Australia
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SLIDE 4
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SLIDE 5

SKA HQ in UK

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SLIDE 6
  • SKA1-LOW
  • 50 – 350 MHz
  • Phase 1: ~130,000 antennas
  • across 40 - 50km
  • SKA1-Mid:
  • 350 MHz – 24 GHz
  • Phase 1: 130 15-m dishes

across 120km

  • Integration of 64 dish MeerKAT

to complete phase 1 array

SKA telescopes in AUS & RSA

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SLIDE 7

SKA Low prototype

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SLIDE 8

Space for SKA

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SLIDE 9

SKA Mid prototype: Foundations

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SLIDE 10

SKA Mid prototype: Panel molds

Picture: CETC54

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SLIDE 11

www.ska.ac.z a

  • SKAO is the central design authority
  • For SKA 1:
  • Dish – The physical dishes, feeds and digitisation
  • SaDT – Signal and Data T

ransport (Included Synchronisation and Timing)

  • CSP – Central Signal Processing (Correlator, Beamformers and Non-imaging

processing)

  • SDP – Science Data Processing
  • INFRA SA
  • INFRA AUS
  • LFAA – Low Frequency Aperture Array
  • TM – T

elescope Manager

  • AIV – Assembly, Integration and Verifjcation
  • FOR the Advanced Instrumentation Program (SKA 2):
  • MFAA
  • WBSPF
  • PAF
  • Consortia are performing element designs

SKA Consortia

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SLIDE 12

www.ska.ac.z a

  • Now preparing for the element and system Critical Design Reviews
  • Starting this year and extending through 2018
  • Creation of a new Inter-governmental Organisation (IGO)
  • Plan is to have agreements for the IGO in place this year
  • Followed by ratifjcation in each member country
  • IGO comes into force early 2019
  • Construction phase begins
  • “CDR T
  • morrow”

SKA: What is next?

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SLIDE 13

1 3

From Alistair McPherson’s presentation at the SKA Engineering Meeting 2017 (and 2016)

“Gentlemen, we have run out of money . It's time to start thinking.” ― Ernest Rutherford

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SLIDE 14

SKA1 construction provisional totals – Phil Diamond SKAO

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€917M  €806M

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SLIDE 15

Updated CCP list (page 1/2)

W S / Origin Descript ion LOW / M ID / COMM ON Science Implication Science Impact 5 .3 9

INFRA_SA Renew able energy t

  • out

er dishes M ID None 1

5 .3

M axim ise use of code produced during Pre-Const ruct ion COM M ON None 1

5 .3 8

Sim plify DDBH LOW LOW None 1

5 .3 8

Sim plify DDBH M ID M ID None 1

5 .2 5 .2

Reduce PSS-M ID: A, 7 5 nodes t

  • 5

nodes M ID Likely none, or sm all reduct ion of pulsar search param et er space. 1

5 .2 5 .2

Reduce PSS-LOW : A, 2 5 nodes t

  • 1

6 7 nodes LOW Likely none, or sm all reduct ion of pulsar search param et er space. 1

5 .3 5

Reduce CBF-M ID: Freq. Slice variant of CSP design vs. M eerKAT-based design M ID None 1

5 .1 9

M ID Frequency and Tim ing Standard: SaDT solution vs. M eerKAT-based solut ion M ID None 1

5 .3 6

M ID SPF Digit isers: DSH solut ion vs. M eerKAT-based solution M ID None 1

5 .2 6/ 5 .2 9

LOW RPF: Early Digit al Beam Form at ion vs. Analogue Beam Form at ion LOW None 1

2

LOW Ant enna: Log Periodic Design vs. Dipole Design LOW None of t he current designs m eet the L1 requirem ents 3

8

SDP- HPC: Deploy 2 Pflops (rat her t han 2 60 Pflops) COM M ON Low er allow ed dut y cycle for HPC- int ensive observat ions. 2

5 .2 4 .3

Reduce Bm ax M ID from 1 5 t

  • 1

2 km : Case A, rem

  • ve 3

dishes, but keep infra t

  • 1

5 km M ID Reduct ion of m axim um achievable resolut ion by 2 %, although can be part ially recovered w it h dat a w eighting and longer int egrat ion tim es. 2

5 .2 4 .2

Reduce Bm ax M ID from 1 5 t

  • 1

2 km : Case B, rem

  • ve infra, but

add dishes t

  • core

M ID Reduct ion of m axim um achievable resolut ion by 2 %, although can be part ially recovered w it h dat a w eighting and longer int egrat ion tim es. 2

5 .2 4 .1

Reduce Bm ax M ID from 1 5 t

  • 1

2 km : Case C, rem

  • ve infra, rem
  • ve dishes

M ID Reduct ion of m axim um achievable resolut ion by 2 %, although can be part ially recovered w it h dat a w eighting and longer int egrat ion tim es. 2

5 .5 .2

Reduce M ID Band 5 feeds: A, from 1 3 to 6 7 M ID Placem ent to be det erm ined based on full com m unit y consultat ion. 2

5 .2 5 .2

Reduce PSS-LOW : B, 1 6 7 nodes t

  • 1

2 5 nodes LOW Likely reduct ion in processed PSS beam num ber (1 .3 x) or pulsar search param et er space 2

5 .2 5 .2

Reduce PSS-M ID: B, 5 nodes t

  • 3

7 5 nodes M ID Likely reduct ion in processed PSS beam num ber (1 .3 x) or pulsar search param et er space 2

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SLIDE 16

Updated CCP list (page 2/2)

8

SDP- HPC: Deploy 1 5 Pflops (from 2 Pflops) COM M ON Low er allow ed dut y cycle for HPC- int ensive observations. 3

5 .3 .0

Reduce Bm ax LOW t

  • 5

km : A, rem

  • ve infra, add 1

8 st ations t

  • core

LOW Science Risk t

  • EoR: Bm

ax. 3

5 .3 .0

Reduce Bm ax LOW t

  • 5

km : B, rem

  • ve 1

8 st at ions LOW Science Risk t

  • EoR: Bm

ax 3

5 .3 a

Reduce Bm ax LOW t

  • 4

km : C, rem

  • ve next

1 8 stat ions LOW Science Risk t

  • EoR: Bm

ax 3

8

SDP- HPC: Deploy 1 Pflops (from 1 5 Pflops) COM M ON Low er allow ed dut y cycle for HPC-int ensive observat ions. 4

8

SDP- HPC: Deploy 5 Pflops (from 1 Pflops) COM M ON Low er allow ed dut y cycle for HPC- int ensive observations. 4

5 .3 1

Reduce CBF-LOW BW : A, 3 t

  • 2

M Hz LOW Longer observing t im es for cont inuum applicat ions (1 .5 x) 4

5 .2 5 .2/ D e e p e r S a v in g s

Reduce PSS-LOW : C, 1 2 5 nodes to 8 3 nodes LOW Likely reduct ion in processed PSS beam num ber (2 x) or pulsar search param eter space 4

5 .2 5 .2/ D e e p e r S a v in g s

Reduce PSS-M ID: B, 3 7 5 nodes t

  • 2

5 nodes M ID Likely reduct ion in processed PSS beam num ber (2 x) or pulsar search param eter space 4

5 .1 3 .2

Reduce Bandw idth out put

  • f band 5

t

  • 2

.5 GHz M ID Longer Band 5

  • bserving t

im es for som e applicat ions (2 x) 4

5 .35

Reduce M ID CBF and DSH BW : 5 to 1 .4 GHz M ID Longer observing t im es to achieve continuum sensit ivit y in Band 5 (3 .6 x) 4

5 .2 4/ D e e p e r S a v in g s

Rem

  • ve 1

1 M ID Dishes from core M ID 1 % Array sensit ivit y loss in core 4

5 .3 0/ D e e p e r S a v in g s

Rem

  • ve 5

4 LOW st at ions from core LOW 1 % Array sensit ivit y loss in core 4

5 .2 4/ D e e p e r S a v in g s

Rem

  • ve addit

ional 1 1 M ID Dishes from core M ID 2 % Array sensit ivit y loss in core 4

5 .3 0/ D e e p e r S a v in g s

Rem

  • ve addit

ional 5 4 LOW st at ions from core LOW 2 % Array sensit ivit y loss in core 4

5 .2 4 .2

Reduce Bm ax M ID from 1 2 t

  • 10

km : D, rem

  • ve infra, rem
  • ve next

3 dishes M ID Lose Science (Planet ary disks, High resolution Star Form ation) 4

5 .5 .1

Rem

  • ve M

ID Band 1 feeds: 1 5 to 0 M ID Lose Science (Cosm

  • logy, Galaxy

Evolut ion) 4

5 .5 .2

Reduce M ID Band 5 feeds: B, from 6 7 t

M ID Lose Science (Planet ary disks, St ar Form at ion) 4

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SLIDE 17

“DCE” ‘proposal’

  • What would happen if we reused as much of MeerKAT as possible?
  • Goal is to have no impact on science
  • Only SKA1 Mid
  • Allowed half of Euro 674 M cost cap
  • Construction starts in 2019…
  • … but we only need to deploy a large scale system by 2022
  • SKARAB2 could be Virtex Ultrascale+ or Stratix 10 with HBM
  • SKARAB2 is a risk mitigation for SKARAB3, which is the preferred

family for SKA in ~2022 timeframe

  • Increase density to 4 devices per 1U
  • Power up to 130W per device, ~23kW per rack
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SLIDE 18

A few key SKA CSP specifjcations

  • Up to 5GHz instantaneous bandwidth (band 5)
  • 130 15m antennas + 64 13.5m MeerKAT antennas
  • Beamformers for:
  • VLBI – up to 4 beams with adjustable bandwidth
  • PSS – search. Up to 1500 beams at 300MHz

bandwidth

  • PST – timing. 16 beams at full bandwidth
  • Correlation
  • 64k channels WB
  • Zoom windows (4, 8, 16, 32, 64, 128, 256 MHz), 16k

channels

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SLIDE 19

SKARAB2 Block Diagram

FAN FAN

QSFP & Cage QSFP & Cage FPGA

FMC FAN FAN

QSFP & Cage QSFP & Cage FPGA

FMC FAN FAN

QSFP & Cage QSFP & Cage FPGA

FMC FAN FAN

QSFP & Cage QSFP & Cage FPGA

FMC PSU FAN FAN

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SLIDE 20

SKARAB2 Hardware Proposal

  • SKARAB vs SKARAB2

S K A R A B S K A R A B 2 E t h e r n e t : 4 x 4 G b E E t h e r n e t : 2 x 1 G b E M e m

  • r

y : 4 G B H M C x 3 M e m

  • r

y : H B M F P G A : 1 x V i r t e x 7 F P G A : 4 x V i r t e x U l t r a S c a l e + D i m e n s i

  • n

s : 1 U D i m e n s i

  • n

s : 1 U P

  • w

e r C

  • n

s u m p t i

  • n

: 1 2 5 W P

  • w

e r C

  • n

s u m p t i

  • n

: 6 8 4 W C

  • l

i n g : F a n A i r F l

  • w

C

  • l

i n g : F r

  • n

t t

  • B

a c k F a n A i r F l

  • w

( T B D )

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SLIDE 21

SKARAB vs SKARAB2 FPGA Specs

SKARAB Virtex 7 (XC7VX690T) 693120 Logic Cells 80 x SERDES

64 used for I/O mezzanine sites @ 10 Gbps 1 used for PCI-E to COM-E module site

1470 x 36Kb RAM Blocks (~52 Mb) 3600 DSP Slices 1927 pins 1000 single ended I/O SKARAB 2 Virtex UltraScale (VU33P/VU35P) 962000-1907000 Logic Cells 32-64 x SERDES

@ 32.75 Gbps

RAM Blocks (~23.6 - 47.3 Mb) UltraRam (90-180 Mb) HBM: 8GB 2880-5952 DSP Slices 208 - 416 single ended I/O 2-5 x 100G Ethernet

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SLIDE 22

SKARAB FPGA Specs in Detail

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SLIDE 23

SKARAB2 FPGA Specs in Detail

SKARAB 2 Virtex UltraScale (VU33P/VU35P – package compatible) 962000-1907000 Logic Cells 32-64 x SERDES

@ 32.75 Gbps

RAM Blocks (~23.6 - 47.3 Mb) UltraRam (90-180Mb) HBM: 8GB 2880-5952 DSP Slices 208 - 416 single ended I/O 2-5 x 100G Ethernet

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SLIDE 24

Thanks

SKA South Africa, a Business Unit of the National Research Foundation, is supervising South Africa’s involvement in the SKA on behalf of the Department of Science & T echnology.