James Webb Space Telescope (JWST) Program Status. Mark Clampin JWST Observatory Project Scientist NASA/Goddard Space Flight Center
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1 James Webb Space Telescope (JWST) Program Status Mark Clampin JWST Observatory Project Scientist NASA/Goddard Space Flight Center
2 James Webb Space Telescope (JWST) Organization Mission Lead: Goddard Space Flight Center Project Scientist: Dr John Mather (Nobel Laureate) International collaboration: ESA & CSA Prime Contractor: Northrop Grumman Space Technology Instruments: Near Infrared Camera (NIRCam) Univ. of Arizona Near Infrared Spectrograph (NIRSpec) ESA Mid-Infrared Instrument (MIRI) JPL/ESA Fine Guidance Sensor (FGS) CSA Operations: Space Telescope Science Institute Description Deployable infrared telescope with 6.5 meter diameter segmented adjustable primary mirror JWST Science Themes Cryogenic temperature telescope and instruments for infrared performance Launch June 2013 on an ESA-supplied Ariane 5 rocket to Sun-Earth L2 5-year science mission (10-year goal) End of the dark ages: First light and reionization The assembly of galaxies Birth of stars and proto-planetary systems Planetary systems and the origin of life 2
3 JWST Sunshield: I UPS Bipod Launch Lock Attachment Points Fixed Spreader Bars at all Locations Momentum Trim Flap Core Region 3
4 JWST Sunshield: II Aft UPS Bipod Launch Lock Attachment Points Momentum Trim Flap Unitized Pallet Structure (UPS) Unitized Pallet Structure (UPS) Telescopic Side Booms 4
5 Sunshield: Deployment Sunshield membrane deployment is now fully managed: sunshield is released and extended one pallet section at a time Each pallet color represents a sunshield section. They are released one at a time during deployment 5
6 Sunshield: Membrane Development 6
7 JWST Mirror Development Flight PM/SM segments are all being figured at Tinsley Primary Mirror Tertiary and Fine Steering mirror ready for delivery to Tinsley 31% B wk 34% C wk 40% B6 19 wk 0% TM 3.2 wk 31% C wk 36% A wk 36% A5 19 wk 37% C4 19 wk 0% B wk 47% A wk 0% SM 3.2 wk 38% A4 19 wk 37% B5 19 wk 39% C1 19 wk 45% A wk 38% A wk 43% C wk 63% EDU / A-PF -L 44.4 wk to PF 0% <1 wk to A1 C7/C-PF -L 49% B wk 44% C wk 44% B wk 0% FSM 40.2 wk 16 wk % COMPLETE RELATIVE TO L3-TINSLEY OPERATIONS SLACK IN WEEKS AGAINST NEED DATE PER M/E AUGUST 2007 MASTER SCHEDULE AT BATC / AXSYS IN HOUSE / L3 EVEN SLICE FIGURE GRIND, FINE SMOOTH OUT POLISH 1% SM/PF -L 48.4 wk COATING (DENTON) FINAL AI&T (BATC) -TINSLEY Secondary Mirror Tertiary Mirror Fine Steering Mirror Mirror sizes to scale 7
8 JWST Mirror Status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light (SM1 / SM2 / SM2) TM Flight (TM1 / TM1 / TM1) 8
9 JWST Mirror Status: III SM Back Surface SM Front Surface ATPL in Preparation of Polishing SM Pathfinder Light and Flight segments have completed machining at Axsys Technologies. Processing is beginning at Tinsley Laboratories. Helium Shroud in Fabrication The helium shroud and regeneration system has been delivered to BATC and tested down to 6K. The Aspheric Test Plate Lens and Illumination Lens is nearing completion at Tinsley Laboratories. Illumination Lens in Optical Test Helium Shroud Installation The SMA Optical GSE Mount and associated hardware has been built and assembled at BATC. (Proof Load Shown) 9
10 EDU Mirror EDU mirror is on schedule for completion of fine polishing this March Cryo-Polish cycle will follow 10
11 Primary Mirror Backplane Pathfinder fabrication: 118 of 153 billets completed through acceptance Piece part fabrication at 46% complete Billets fabricated include V1 and drop tubes, flat plates and two T300 latch plane V1 tubes Flight fabrication: 34 of the 184 total flight center section billets are through cure Overall center section piece part fabrication at 3% C4 A4 11
12 NIRCam ETU Hardware ZnSe Collimator BaF 2 Camera Bench panel after anodizing Filter Wheel Drive Board Focus Mech Drive Board Instrument Control Electronics 12
13 NIRSpec ETU/Qual Model Hardware Fore Optics Focal Plane Assembly Optical Bench 13
14 FGS Hardware Demo Unit Focal Plane Primary Mirror Blank ETU Guider Optical Bench Prototype Etalon ETU Guider Secondary Mirror 14
15 MIRI Verification Model Performing gravity sag test at the Rutherford Appelton Lab, UK 15
16 ISIM Subsystems ISIM Electronics Compartment Demo Model ICDH ETU SpaceWire Card ISIM Structure Thermal Distortion Test Article 16
17 ISIM Structure Harness Mockup Currently in Bldg 29 17
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