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General strategy for the AIV during Phase A • 2 roadmaps have been identified to prove the AIV feasibility of the 32 telescopes 1. INDUSTRY 1. Paper study concerning the aspherical lenses procurement feasibility on a ~2 years time schedule 2. Paper study concerning the spherical lenses procurement feasibility on a ~2 years time schedule 3. Paper study concerning the albemet structure procurement feasibility on a ~2 years time schedule 2. RESEARCH INSTITUTES 1. Identify an AIV concept and procedure, defined in agreement with the industry 2. Test on a TOU BraedBoard of the AIV procedure 3. Test on the prototype of the warm/cold system performance, defined and performed together with the industry TOU Alignment Concept Variable Iris Beam Expander B/S Focussing CCD Laser Back Reflected Light Transmitted Light Focussing CCD Telescope By using Airy and Newton rings both of the back reflected and of the transmitted light (introducing one lens at a time) the alignment will be performed; to maximize fringe contrast and airy rings visibility: 1. the detectors are conveniently mounted on linear stages which can move along the optical axis 2. light shields can be inserted between each lens, to isolate the back reflected light, when needed, coming only from that lens 3. A variable diameter iris is inserted on the collimated beam, to maximize the transmitted and back-reflected spot visibility TOU Alignment Set-Up: Vertical Focussing CCD Transmitted Light To allow lenses insertion from the top, the final alignment set-up for the BB will be vertical TOU Variable Iris Beam Expander B/S Laser Back Reflected Light Focussing CCD Strategy for the prototype alignment 1. 2. PRE-BreadBoard: Identification of commercial lenses with, as much as possible, the same curvature of the final design lenses, with the aim to build a pre-prototype (completely realized with commercial parts) to: test the alignment procedure and learn from the test setup (Airy and Newton rings visibility, decenter and tilt misalignment sensitivity, tuning of the test setup components, like for example the movement range of the detectors) BreadBoard: Realization of an “equivalent mechanical structure” (in term of thermal behaviour) to perform the real final alignment procedure and eventually test also in cold conditions the optical performance of the system. This phase will be performed with a set of lenses as close as possible to the final design lenses, differing only for the glasses and for the usage of a spherical lens instead of the aspherical one TOU Pre-BreadBoard Variable Iris Beam Expander B/S Focussing CCD Laser Back Reflected Light Transmitted Light Focussing CCD Pre-BreadBoard, realyzed with commercial lenses and commercial XYZ and Tip-Tilt adjustments for each lens TOU BreadBoard Focussing CCD Frame connected to the bench, allowing the “TOU Dummy” rotation for lenses insertion from the top and their alignment similarly to what would happen with the final structure Transmitted Light Fixing points TOU Dummy Structure Rotating points Variable Iris Beam Expander B/S Laser Back Reflected Light Focussing CCD TOU Bradboard test • Preliminary discussions with the industry have outlined this possible strategy for the TOU prototype test: – Warm test (Research institutes): being the alignment performed in warm conditions, a few test on the expected TOU “warm performance” are foreseen: 1) a test of the PSF quality on axis 2) an interferometric test of the TOU optical quality – Cold test (Research institutes + Industry): in a climate chamber operating in vacuum at the required temperature (-80º), we will perform: 1) a test of the PSF optical quality on axis 2) an optical quality test (interferometric or Hartmann test) 1) TOU PSF Test in warm Performed by the Research Institutes Tip-Tilting Flat Folding Mirror Collimated Beam Test Camera, adjustable in focus Off Axis Parabola Vis Illuminator Optical Fiber 2) TOU Optical Quality Test in warm Performed by the Research Institutes Zygo GPI FP F/1.5 Transmission Sphere 4" - 1/10 Wave, P-V DYNAFLECT Coated TOU Cold Test Critical Items • Problems due to the low testing T and to the gradient between inside and outside the Climate Chamber: T~+20º Lens effect Shrinking effect “Lens Effect” of the Input Optical Window Enlarging effect – The input optical window of the Climate Chamber is affected by aberrations (“lens” effect) – If the test requires auxiliary optical components inside the chamber, they will also be affected by aberrations and particular care shall be given to Climate Chamber their mounts Input optical window Ambient T~-80º Flat ideal shape TOU Cold Test strategy • Characterize the Input Optical Window aberrations • In any case, to minimize the lens effect of the Input Optical Window, better to use parallel beams setup at the climate chamber entrance • Better NOT to use additional optics inside the climate chamber • If additional optics inside the chamber is needed, better to use flat mirrors instead of concave mirrors, again to minimize the “lens effect” • 4 test proposed, but we are converging on test 1 and 2c, which require only one crygenic stage and no optical elements inside the climate chamber 1) TOU PSF Test on axis in cold Performed by the Research Institutes + Industry Climate Chamber (T~-80º) Input optical window Flat Folding Mirror Collimated Beam Test Camera remotely adjustable in focus Off Axis Parabola Advantages: • Parallel beam in input • No additional optical parts inside the chamber • Only 1 “cold” motoryzed axis required Optical Fiber Vis Illuminator 2a) TOU interferometric cold test I Performed by the Research Institutes + Industry F/1.5 transmission sphere Climate Chamber (T~-80º) Interferometer Input optical window Disadvantages: • No Parallel beam in input • Additional optical parts required inside the chamber • 2 “cold” motoryzed axis required Advantages: • The required optical element inside the chamber is a flat mirror Flat Mirror (TT remotely adjustable) 2b) TOU interferometric cold test II Performed by the Research Institutes + Industry Climate Chamber (T~-80º) Collimated Beam Interferometer Input optical window Concave Mirror F/1.5 (TT & Focus remotely adjustable) Disadvantages: • Additional optical parts required inside the chamber • The required optics inside the chamber is a fast concave mirror (“lens effect”) • Three “cold” motoryzed axis Advantages: • Parallel beam in input 2c) TOU Hartmann test in cold Performed by the Research Institutes + Industry Hartmann Mask Climate Chamber T~-80º Collimated Beam P1 Off Axis Parabola Input optical window P2 CCD (movable in focus) Advantages: - Parallel beam in input - No other Optical Parts Vis Illuminator inside the chamber - Only 1 “cold” motoryzed axis required Knowing with precision the relative position of P1 and P2 (linear stage with encoder), we can know very precisely where is the TOU focus and measure the optical quality in term of Encircled Energy, even without going with the CCD there! Optical Fiber Status • The procurement of all the opto-mechanical components needed for the Pre-BB, for the BB, for the lab setup, for the “warm” and “cold” test has started and all the order have been placed since mid November 2010 • The industrial studies are about to be placed in these days, hopefully all before the end of 2010, at latest in January 2011 Time planning • Pre-Breadboard – Opto-Mechanical components arriving 15/20 Jan 2011 – Alignment test results by end of Jan/mid Feb 2011 • TOU Breadboard – Opto-Mechanical and test components arriving by 31 Mar 2011 – “Warm” alignment and test of the TOU prototype by 15 Apr 2011 – “Cold” test in Galileo by 25 Apr 2011 – Test report by 30 Apr 2011 • This planning has no contingency present and it is based on the best effort delivery date of SESO; a shift ranging from 1 to 4 weeks could easily happen Items TBD with Daniele • • • • • • • • • • Light shields between each lenses (TOU) Tools for lenses insertion (TOU&Dummy) Tools (3 screws at 120deg) for lenses alignment (TOU&Dummy) Reasonable machining precision in Z for the barrel and for the lenses mounts (TOU&Dummy) Spacers for focus? Travel for XY adjustment (1mm?) How do we hold and rotate the structure (Dummy) At which minimum height will be the Optical Axis (Dummy) Detector connection (Linear Stage) How do we connect the lenses to their mounts? Glue? From preliminary discussion with the industry, issue with the test in vacuum for the glue degasing… Who will in case glue the lenses for the prototype?