Dear collaborators; Here is the agenda and suggested speakers of the module review in Dec. 4(Mon). If the speaker can not make the presentation, please arrange a speaker for him/her. Appended is the minimum required info (as well as the full list of info for the reference) which the convenors regard as critical. In the latter half of the review, we require critical info from the collaborators working on the different module styles and electronics. We expect full cooperation of each sectors to the reviewers, who may request separately with his due date of the info. Hope we can work hard and make the review successful, in turn, the project itself. Y.Nobu Unno and Tony Carter P.S. Agenda etc can be accessed in the Web, http://arkhp1.kek.jp/~unno/SCTSGmod.html. ______________________________________________________________________________ December Module Review ______________________ Chair : N Unno (1) Thermal measurements - rphi style H Iwasaki 25min - Z style D Howell 25min (2) Thermo-mechanical analysis - FEM G Tappern 20min - Measurement plan R Nickerson 20min ----- BREAK ---- Chair : A Carter (1) Electrical Performance H Sadrozinski 30min (2) Radiation length assessment R Apsimon 20min (3) Forward Module design issues N Jackson 20min ______________________________________________________________________________ The minimum required info. - Thermal measurements 3.1 Temperature profile across a complete (thermal) module, mounted on a realistic cooled support, for constant power in silicon and chip (see specifications). The measurement should be made with the coolant temperature approximately equal to the ambient air temp.(e.g., the room temp. or controlled 0 degC, 20 degC, ...) and +-10degC higher/lower. 3.2 Reproducibility of the thermal contact to the cooling element. The measurement (3.1) should be obtained for several modules mounted on a common structure. If this is not possible one or two modules should be repeatedly mounted on the structure (e.g., 5 times) and temperature profile variations obtained. - Thermo-mechanical analysis FEM analysis results are to be presented on both the z-style and the rphi-style. The measurement plan is to layout the plan to provide the distortion measurements for both styles by the March/April review. - Electrical performance 1.1 Noise measurements on fully bonded 12 cm strip. Compare with the noise on no-bond and extract the noise due to making the module. Please indicate detector geometry, technology, and configuration. 1.2 Second noise measurment on two consecutive triggers. The measurmet should be done on data from the second trigger, as a function of the delay between the two. The delay should cover the range of digitization time of the first trigger. 1.3 Bond position dependence (applies to Z module) compare noise of first and last strip to middle strip in order to separate fan-out/in effect from bond position effect (strip series resistance, fan-out length, glue length). 1.4 Delay Curve: vary calibration pulse with respect to pipeline clock to check for pickup effects (see talk of H.Sadrozinski in Oxford module group meeting). 1.6 Capacitance measurements of fan-out/in (versus fan-out/in strip length). Results for alumina, beryllia and CVD diamond, if possible. Compare the noises due to the fan-out/in with the results obtained for (1.1) and (1.2) (e.g., noises of the 2 chip APV5 Z module and the FELIX128, 4 chip Z module). - Radiation length For existing modules (rhi and z), and for the final ATLAS modules (rphi and z) for the configuration of Binary and Analog/Digital readouts, 2.1 Provide spreadsheet of all materials used and properties, including the additional support needed for mechanics and cooling. 2.2 Calculate radiation lengths of all materials and components locally and averaged over a 6x12 cm area. =================================== Full list of the module selection criteria (available on the Web, http://arkhp1.kek.jp/~unno/SCTSGmod.html, together with the module spec, etc.) Module Selection Criteria (Updated: 1995/11/3) (1) Electrical performance (Noise, ...) 1.1 Noise measurements on fully bonded 12 cm strip. Compare with the noise on no-bond and extract the noise due to making the module. Please indicate detector geometry, technology, and configuration. 1.2 Second noise measurment on two consecutive triggers. The measurmet should be done on data from the second trigger, as a function of the delay between the two. The delay should cover the range of digitization time of the first trigger. 1.3 Bond position dependence (applies to Z module) compare noise of first and last strip to middle strip in order to separate fan-out/in effect from bond position effect (strip series resistance, fan-out length, glue length). 1.4 Delay Curve: vary calibration pulse with respect to pipeline clock to check for pickup effects (see talk of H.Sadrozinski in Oxford module group meeting). 1.5 Signal quality: probe digital signals on hybrid for reflections, risetime, delays, skewing at different positions on the hybrid. 1.6 Capacitance measurements of fan-out/in (versus fan-out/in strip length). Results for alumina, beryllia and CVD diamond, if possible. Compare the noises due to the fan-out/in with the results obtained for (1.1) and (1.2) (e.g., noises of the 2 chip APV5 Z module and the FELIX128, 4 chip Z module). (2) Radiation length For existing modules (rhi and z), and for the final ATLAS modules (rphi and z) for the configuration of Binary and Analog/Digital readouts, 2.1 Provide spreadsheet of all materials used and properties, including the additional support needed for mechanics and cooling. 2.2 Calculate radiation lengths of all materials and components locally and averaged over a 6x12 cm area. 2.3 Provide a list of adhesives: cure schedules, glass transition temperatures, radiation hardness if known. 2.4 Provide a list of encapsulants: cure schedules, radiation hardness (3) Thermal performance 3.1 Temperature profile across a complete (thermal) module, mounted on a realistic cooled support, for constant power in silicon and chip (see specifications). The measurement should be made with the coolant temperature approximately equal to the ambient air temp. (e.g., the room temp. or controlled 0 degC, 20 degC, ...) and +-10degC higher/lower. The results should be compared with a corresponding finite element analysis. 3.2 Reproducibility of the thermal contact to the cooling element. The measurement (3.1) should be obtained for several modules mounted on a common structure. If this is not possible one or two modules should be repeatedly mounted on the structure (e.g., 5 times) and temperature profile variations obtained. 3.3 Simulation of runaway: use feedback on embedded wires, or use irradiated detectors, compare the results with a finite element analysis. (4) Mechanical performance (See "Module Specification" for tolerance numbers) 4.1 Measurement of thermally induced distortions. This should be measured with an instrument (preferably of the non-contact type) with a resolution in the bending plane of better than or equal to 10 microns. Measure distortion as a function of chip power, detector power, and possibly coolant and ambient temperatures (+20, +10, 0, -10degC), and compare with finite element results. The distortion should be measured for non-uniform heating, e.g., roofing in the f direction. 4.2 Reproducibility of the module placement accuracy that can be (regularly) achieved for modules on staves and cylinders. 4.3 Extreme thermal cycle: -20 --> +70 degC ten times. 4.4 Detailed assembly procedures should be provided, with suitable drawings, for both the current H8 modules and future planned designs. Estimates should be given of the alignment accuracy achieved against the design values. the reasons for discrepancies should be outlined. 4.5 If high temperature steps are used in module assembly document changes which occur. 4.6 Wire bonding: demonstrate bondability, total number of bonds - Are all surfaces compatible? reworkable? - Are there problems with vertical steps or excessive length bonds? - Stiffness and deformation of components which are bonded - Specify wire diameter - Encapsulation (is the encapsulant reworkable? radiation hard?) (5) Cost aspects 5.1 List of special fixturing or tools needed 5.2 Time estimates for assembling and testing 5.3 Estimates on assembly yield 5.4 Document cost of components and manpower. (6) Construction aspects 6.1 Document mounting arrangement on to the support element 6.2 Document services and connectivity 6.3 Document repairability 6.4 Document safety issues and use of hazardous materials