The James Webb Space Telescope

The James Webb Space Telescope Jonathan P. Gardner NASA’s Goddard Space Flight Center http://jwst.nasa.gov Space Science Reviews, 2006, 123/4, 485 1...
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The James Webb Space Telescope

Jonathan P. Gardner NASA’s Goddard Space Flight Center http://jwst.nasa.gov

Space Science Reviews, 2006, 123/4, 485 1

James Webb Space Telescope Integrated Science Instrument Module (ISIM)

• • • • •

6.6m Telescope Successor to Hubble & Spitzer. Demonstrator of deployed optics. 4 instruments: 0.6 to 28.5 μm Passively cooled to < 50 K.



Named for 2nd NASA Administrator

Secondary Mirror

Spacecraft Bus

• • • • • •

Primary Mirror

5 Layer Sunshield

Complementary to GMT, ALMA, WFIRST, etc NASA + ESA + CSA: 14 countries Lead: Goddard Space Flight Center Prime: Northrop Grumman Operations: STScI Senior Project Scientist: Nobel Laureate John Mather 2

Long Fairing 17m

Upper stage

Ariane V launch Kourou, French Guiana

H155 Core stage

Video

P230 Solid Propellant booster Stowed Configuration

4

Video

5

Wavefront Sensing and Control OTE Deployment / First Light (Image Mosaic)

SM Focus Sweep Segment Identification

NIRCam First Light

After Segment-Image Array

Commissioning

Segment Search

After Global Alignment

Segment-Image Array DHS (20 edges)

Global Alignment After Image Stacking

Image Stacking

After Coarse Phasing

Coarse Phasing (DHS) Single Field Fine Phasing Pupil Imaging

After SF Fine Phasing

Multi-Field Fine Phasing Wavefront Monitoring & Maintenance

JWST

Fine Phasing on JWST Testbed Telescope Clearly (repeatedly) Demonstrates Coherent Image Addition

116 nm rms

• Double Pass Phase Retrieval Estimate - ~0.95 Strehl ratio - (single pass at 1550 nm on TBT - Flight requirement is >0.8 Strehl @ 2micron •

Stacked Point Spread Function (left) contains random small tip/tilt and piston errors (Before)



Phased PSF clearly indicates coherent addition and success of closed loop fine phasing (After)

• 1/6 scale test-bed Telescope

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Near-Infrared Camera

Lockheed Martin industrial partner

University of Arizona PI: Marcia Rieke Teledyne HgCdTe detectors

• Simultaneous observing at two wavelengths over 2.3’ x 4.6’ FOV.

Long Wavelength Detectors

Short Wavelength Detectors

Pick-off Mirror

• 7 Broad-band filters over 0.6 < λ < 5.0 m • Additional medium and narrow-band filters

Dichroic

• Filter wheels include wavefront sensing hardware. Filter Wheels

• Coronagraphy NIRCam 8

Near-Infrared Camera

Go Girl Scouts

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Near-Infrared Spectrograph

ESA instrument EADS Astrium prime contractor



Multi-Object Spectroscopy

GSFC providing microshutters and detectors

– Micro-shutter array – 3.4’ x 3.4’ FOV.

• •

IFU, 3’’ x 3’’ R=1000 & R=3000

Video

– 3 gratings cover 1.0 < λ < 5.0 μm



R=100 Prism – 0.6 < λ < 5.0 μm

Flight NIRSpec Micro-Shutters: 730 x 342 array of 203 x 463 mas pixels Flight Microshutters Integrated into Instrument 10

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European consortium George Rieke, US Science Lead Gillian Wright, EC Science Lead

Mid-Infrared Instrument

JPL providing detectors, cooling, management



Broad-band Imaging

– –

5 < λ < 27 μm 1.4’ x 1.9’ FOV



R=3000 IFU

– –

5 < λ < 28.5 μm 3” x 3” FOV

ETU First Light •

R = 100 Slit –

Flight MIRI at GSFC

• •

5 < λ < 10 μm

Coronagraphy Cryocooler to 7K

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MIRI Installation into ISIM

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Flight Fine Guidance Sensor Near-Infrared Imager and Slitless Spectrograph

Com Dev industrial partner

CSA contribution

 Broad-band guider (0.6 – 5 microns)  Science imagery:

Flight FGS

– Slitless spectroscopic imagery (grism) ‐ R ~ 150, 0.8 – 2.25 microns optimized for Ly alpha galaxy surveys ‐ R ~ 500, 0.7 – 2.5 microns optimized for exoplanet transit spectroscopy

– Sparse aperture interferometric imaging (7 aperture NRM) 3.8, 4.3, and 4.8 microns

 Field of view: 2.3 x 2.3 arc minutes  Angular resolution (1 pixel): 68 mas  Detector type: HgCdTe, 2048 x 2048 pixel format, 3 detectors 14

FGS Delivery

JWST.ISIM.AUG.MSR

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Video

16

Operations

• STScI has been designated as Science Operations Center

JWST at L2

Astronomer

Ka

S

• GO, Treasury and GTO programs similar to HST

STScI

TAC

DSN 17

JWST’s Flight Mirror Status

JWST

Flight mirrors arriving at GSFC

JWST

All mirrors are gold-coated

Gold Coatings Exceed Requirements Measured PM Run Reflectance  (Visible / Near IR spectrometer  6 degree AOI) 99.5 99 98.5 Reflectance (%)

98 97.5 97 96.5 96 95.5 95 94.5 94 800

1000

1200

1400

1600

1800

2000

2200

2400

Wavelength (nm) A1

A2

A3

A4

A5

A6

B2

B3

B5

B6

B7

B8

C1

C2

C3

C4

C5

C6

C7

PM Average

Reqt

JWST Mirror Fabrication Raw Be billet (two mirrors)

JWST Mirrors made of beryllium Lightweight and stable at 40 K Brush-Wellman Primary segment Secondary

Tertiary

Machined & lightweighted by Axsys 92% material is removed

Mirrors polished at Tinsley Segment cryo-figure: 20 nm

Ambient Surface Figure JWST

Cryo Surface Figure

Flight Mirror Status • All flight primary mirrors completed w/gold coating  Acceptance

testing completed

Video

Flight Mirror A4 in acceptance vibe • Mirror segments are now being

Mirror Segments Complete: - Cryogenic optical test (post-vibe) meets WFE requirement.

built up with actuators on the back for installation onto backplane. • Flight mirror fabrication program completed in 2011 JWST/Clampin/Observatory Status

JWST

Video

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JWST Secondary Mirror

Flight Secondary Delivered to GSFC JWST

Tertiary Mirror coated with gold!

JWST

Aft-Optics System

Predicted Image Quality: 2 μm & 4 μm

JWST

Predicted Image Quality: 0.7 μm & 1 μm

JWST

ISIM Flight Structure Completed

Structure in SES after Cryoset Test Complete

JWST_ISIM.June.MPR/34

OSIM/ISIM:  The Show has Begun

Webbcam

Live update every 60 seconds  http://www.jwst.nasa.gov/webcam.html.

Webbcam

Live update every 60 seconds  http://www.jwst.nasa.gov/webcam.html.

Pathfinder Center Section Bonding Complete

JWST

Wings complete

JWST

1/3rd Scale Sunshield

JWST

Sunshield Status Status as of: 03/31/12

PROJECT: JWST



Nexolve/NGAS making good progress on template work

Template Layer 5 “cup down” under 3X loading JWST.ISIM.APR.MSR

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Sunshield Deployment Testing

Observatory level cryo-vacuum testing will occur at the Johnson Space Center in Houston

JSC Chamber A

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Want to Learn More about JWST?

2007 Conference Proceedings Available on Amazon Gardner et al. 2006, Space Science Reviews, 123/4, 485 http://jwst.nasa.gov/scientists.html

White Papers: JWST in Decadal Survey Solar System Objects Dark Energy Transiting Planets Coronagraphy Planetary Systems Stellar Pops Star Formation Galaxy Assembly First Light Astrobiology Scientific Capabilities Observation Planning

Science White Papers http://www.stsci.edu/jwst/science/ 46

Workshop on “Frontier Science Opportunities with JWST” • • • • • •



June 6-8, 2011 STScI Baltimore, Maryland, USA www.stsci.edu Webcast and charts: https://webcast.stsci.edu/webcas t/searchresults.xhtml?searchtype =20&eventid=147&sortmode=1 See white paper for summary: http://www.stsci.edu/jwst/science

jwst.nasa.gov

Latest News Project Milestones updated monthly

Social Media www.stsci.edu/jwst

Astronomy Software Tools ETC, PSF, APT

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The James Webb Space Telescope

Jonathan P. Gardner NASA’s Goddard Space Flight Center http://jwst.nasa.gov

Space Science Reviews, 2006, 123/4, 485 49

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