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EXPANDING THE FRONTIERS OF SPACE ASTRONOMY The James Webb Space Telescope Massimo Stiavelli July 22 nd , 2019

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Page 1: EXPANDING THE FRONTIERS OF SPACE ASTRONOMY

EXPANDING THE FRONTIERS OF S PACE AS TRONOMY

The James Webb Space Telescope

Massimo Stiavelli

July 22nd, 2019

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Plan of the talk

• The James Webb Space Telescope

• Observing plans and opportunities

• JWST status

Page 3: EXPANDING THE FRONTIERS OF SPACE ASTRONOMY

Plan of the talk

• The James Webb Space Telescope

• Observing plans and opportunities

• JWST status

Page 4: EXPANDING THE FRONTIERS OF SPACE ASTRONOMY

We need a newer and bigger telescope

JWST is an international collaboration between NASA, ESA and CSA

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What will JWST do after it’s launched?

Attempt to find and characterize Earthlike planets in the Habitable zone

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HST UDF

Simulated JWST Image

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Summary of JWST instrument capabilities

jwst.stsci.edu/instrumentation

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Spectroscopy and JWST

JWST has many spectroscopic capabilities:

• NIRSpec supports MOS, IFUs, and single slit spectroscopy

• NIRcam supports slitless spectroscopy

• NIRISS support slitless spectroscopy and single object slit spectroscopy

• MIRI supports IFU spectroscopy and low-res slit spectroscopy

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Near Infrared Camera – NIRCam (US)NIRCam Capabilities2 channel imager from λ = 0.6 to 5.0 microns, get λ < 2.5 & λ > 2.5 micron

simultaneously

Nyquist sampling of diffraction limit at 2 microns (0.032”/pixel) and 4 microns

(0.065”/pixel)

2.2’ x 4.4’ field of view

Short and long wavelength coronagraphy

Slitless spectroscopy for λ = 2.4 – 5.0 micron

Check NIRCam pocket guide: jwst.stsci.edu/instrumentation/nircam

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Near Infrared Spectrometer – NIRSpec (ESA)

NIRSpec CapabilitiesNear Infrared wavelength coverage of λ = 0.6 to 5.0 micronsThree different spectral resolutions of R = 100, 1000, and 2700Modes: Single Slit Spectroscopy (slits with 0.4” x 3.8”, 0.2” x 3.3”, 1.6” x 1.6”)

Integral Field Unit (3.0” x 3.0”)Multi Object Spectroscopy (3.4’ x 3.4’ with 250,000 - 0.2” x 0.5” microshutters)

Check NIRSpec pocket guide: jwst.stsci.edu/instrumentation/nirspec

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NIRSpec enables multi-object spectroscopy

248,000 microshutters!

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Mid Infrared Instrument – MIRI (US-EC)

MIRI CapabilitiesHigh resolution imager with sensitivity from λ = 5 to 28 microns, 10 broad-band filtersλ = 5.0 to 28.3 microns with 0.11” pixels1.23’ x 1.88’ field of view Coronagraphy at 10.65, 11.4, 15.5, and 23 microns (24” to 30” field of view)Integral Field Unit with R = 2200 to 3500, at 4 wavelengths (image slices 0.18” to 0.64”)Single Slit Spectroscopy from 5.0 to ~14 microns in 0.6 x 5.5” slit (R ~ 100 at 7.5 microns)

Check MIRI pocket guide: jwst.stsci.edu/instrumentation/miri

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Near Infrared Imager and Slitless Spectrograph – NIRISS (CSA)

NIRISS Capabilities

Imaging - λ = 0.9 to 5.0 microns over a 2.2’ x 2.2’ field of view with 0.065” pixelsWide Field Slitless Spectroscopy - λ = 1.0 to 2.5 microns at R ~ 150Single Object Slitless Spectroscopy - λ = 0.6 to 2.5 microns at R ~ 700Aperture Mask Interferometry - λ = 3.8 to 4.8 microns, enabled by non-redundant mask

Check NIRISS pocket guide: jwst.stsci.edu/instrumentation/niriss

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JWST Point Source Sensitivity

Data cube-based ETC available on the web

Page 15: EXPANDING THE FRONTIERS OF SPACE ASTRONOMY

Plan of the talk

• The James Webb Space Telescope

• Observing plans and opportunities

• JWST status

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16

7/27-8/7/2020

GO Cy1 TAC

Commissioning

(L+6 mo.)

(L+6)

Cycle 1 obs. begin

JWST Science Planning Timeline (July 2019)

2018 2019 2020

5/1/2020

GO Cy1

prop. due

L+11

GO Cy2 Call

2021

Cycles 1 & 2 Call for Proposals

6/25/2019

GTO and ERS Cy1 APT

files submitted

DD ERS observations

2022

L+9

GTO Cycle 2 deadline

1/23/2020

GO Call re-opened

L+13

GO Cy2 deadline

L+15

GO Cy2 TAC

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• Astronomer’s proposal tool (APT)

• Exposure time calculator (ETC)

• Quantitatively validated with instrument teams

• Runs on Amazon Web Services to guarantee scalability and adequate CPU resources

• Calibration pipelines

• More sophisticated than those on HST after 25 years in operations

• New JWST Help Desk portal

• Web-based, includes comprehensive documentation search and user forum.

• User documentation (JDOX)

• Wikipedia-style integrated web documentation

• Data analysis tools

• Many new applications, including spectroscopic viewer, multi-object and IFU tools

• Written in Python and integrated with Astropy

• Data simulators

• STIPS imaging simulator to be released

JDOX

JWST ETC

JWST User Tools

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Plan of the talk

• The James Webb Space Telescope

• Observing plans and opportunities

• JWST status

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James Webb Space Telescope status

We have three months of schedule reserve to a launch date at the end of March 2021

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James Webb Space Telescope status

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Technical progress

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OTIS completed cryovac testing at JSC

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ISIM backside at NGAS : a radiator deployment test

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Aft sunshield UPS deployment

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Preparations for sunshield deployment test

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Diving board inspections

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James Webb Space Telescope status

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James Webb Space Telescope status

Flight control room during the Ground Segment test 2

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JWST is still planned for a March 2021 Launch

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Conclusions

• JWST is now planned for launch in 2021

• The instruments and optics (ISIM) have completed and passed their final test.

• There are no know technical issues. Aside for the complexity of the observatory and its consequent vulnerability to human errors.

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Lessons learned from JWST, HST/ACS, HST/WFC3, VLT

• Design and planning• Reuse with modifications doesn’t exist

• Reserves are important (time and money)• Any dollar not spent when needed, will cost 2-3 dollars in the future

• Materials are cheap, people are not – e.g. WFC3 pins• How does your mission cost compare to its weight in gold?

• Simplicity and common sense – e.g. ACS camera head, WFC3 UVIS channel

• When complexity is unavoidable• focus on interfaces and clear communications

• Lots of simple things put together are complex

• Develop a design reference mission

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Lessons learned from JWST, HST/ACS, HST/WFC3, etc

• Implementation• Hard parts are hard but simple things are also hard - e.g. thrusters

• It pays to have a system scientist i.e. the science analog of a system engineer, who worries about beginning to end science flow – e.g. VLT “Porsche” manager, LEP

• Balance between descopes and new requirements• System engineers can use the design reference mission to guide choices, assess mechanism

lifetime etc.

• When in doubt, document it

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E X P A N D I N G T H E F R O N T I E R S O F S P A C E A S T R O N O M Y