Space Grant Consortium - University of Wisconsin - Green Bay

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Detector Array and ROIC SCA Mount Levels of FPA Structure SCA with Flex Cable 62
B. FPA Material Comparison The FPAs of JWST all share the same core components. Each FPA, however, is its own version of the shared design. These versions utilize different materials for some components. The ROIC for all the FPAs is made of silicon because it is an integrated circuit similar to one used for a computer chip. The SCA mount is made of a TMZ Molybdenum hybrid for all the instruments, except MIRI which uses a copper alloy. These were chosen because they provide good coefficient of thermal expansion (CTE) match with the ROIC. The interface plate between the SCA mount and mosaic plate is also made of Molybdenum for similar purposes. The three flexure struts, which also serve as standoffs, that connect the mosaic plate to the baseplate are made of Titanium. The struts accommodate thermal mismatches and provide active temperature control. The baseplate is made of Titanium, Molybdenum for MIRI, and provides a strong base for the assembly. The assembly housing for radiation shielding and shadow mask stray light mitigation are unique to each FPA. [3][11] NIRSpec FPA NIRCam FPA MIRI FPA FGS FPA [16][17][8][4] 63
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Space Grant Consortium wisconsin UN
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THE CASSINI ENCOUNTER WITH THE GEM
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Th he proceedinngs of our 199th Ann
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Wisconsin Space Grant Consortium Un
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Part 3: NASA Reduced Gravity Progra
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EAA Women Soar - You Soar, Lee Siud
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Elijah High Altitude Balloon Projec
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Our experience with the HALO II lau
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which had been a problem in the pas
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Figure 6: 3-D GPS Generated Track o
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Results The seeds tested in the lab
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hour as we assumed the flight in th
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Experimental Results There are two
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A series of tests were done in a co
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380 360 340 320 23.3 Temp. (Celsius
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First Place, Non-Engineering: Schmi
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of the basis for fin designs came f
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ejection charge from the motor fire
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using rip-stop nylon cloth. To atta
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Post-flight recovery. A field searc
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Thus, it is believed that the main
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[2] Public Missiles Ltd. Frequently
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Design Features The chief requireme
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The joint between the dart and the
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Area dramatically influenced by flo
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Altitude [ft] 6000 5000 4000 3000 2
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though a strong crosswind was prese
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Our Design Our rocket uses the basi
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e easily recovered. Bong recreation
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Performance Characteristics of Pred
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Background and Context: Student Roc
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The Rocky Mountain Miners’ compet
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19th Annual Conference Part Three N
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The angle of repose of a granular m
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Experiment Design The experiment co
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on the ground and in the Weightless
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measurements for the 1 − g data.
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[ImageJ, 2008] Image Analysis Softw
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Dynamics Characterization of the El
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Figure 1 - A calibration equation f
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Wire A secondary investigation into
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[1] Taminger, K. M. B.; and Hafley,
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Introduction The analysis of wake v
Page 96 and 97: Figure 2: Screen I mage o f G UI. T
Page 98 and 99: References ¹ Burnham, D.C., and Ha
Page 101 and 102: Validation of Novel Rigid Body Fric
Page 103 and 104: forces is implemented in the popula
Page 105 and 106: Figure 2. CAD representation of a t
Page 107 and 108: Results Figure 5. Assembled hydraul
Page 109: References Anitescu, M. (2006). "Op
Page 112 and 113: Multi-stage Joule-Thomson cycles ar
Page 114 and 115: significant change in total compres
Page 116 and 117: The enthalpy (h3) of the 2 nd stage
Page 118 and 119: UA m� ⎛ ε −1 ⎞ ( c nd c st
Page 120 and 121: educed, the temperature range that
Page 122 and 123: 7. Lemmon, E. W.; Huber, M. L.; McL
Page 124 and 125: Throughout each of the run cycles,
Page 126 and 127: and heater adjusted to accommodate
Page 129 and 130: Phaeton Mast Dynamics Mechanical Sy
Page 131 and 132: exposure to the FEMAP with NASTRAN
Page 133 and 134: The irregularity in the plots above
Page 135 and 136: inversion of a particular matrix, t
Page 137: clarified. Additionally, the PMD ki
Page 140 and 141: A. Abstract For hardware to be flig
Page 142 and 143: should be performed at the JWST obs
Page 144 and 145: B. Attenuation and Uncertainty Shoc
Page 148 and 149: Detector Shock Environment The leve
Page 150 and 151: Orbiter (MRO), Moon Mineralogy Mapp
Page 152 and 153: 4. NASA JPL. MIRI FOCAL PLANE SYSTE
Page 155 and 156: Is Lake Superior a significant sour
Page 157 and 158: each grid cell at daily resolution.
Page 159 and 160: Figure 3. (a) Seasonal cycle of lak
Page 161 and 162: Figure 5. Model pCO2 at the surface
Page 163: Marshall, J., A. Adcroft, C. Hill,
Page 166 and 167: numerical weather prediction (NWP)
Page 168 and 169: High Resolution Radiometer (AVHRR)
Page 170 and 171: On the morning of 26 May 2008, ther
Page 172 and 173: References Behnke, C., 2005: Synopt
Page 174 and 175: Figure 3 Figure 3 contains base ref
Page 177 and 178: A Comparative Study of Type IIb Sup
Page 179 and 180: Fig. 3.— Cartoon Image of SN blas
Page 181 and 182: Fig. 4.— Light curve of SN 2008bo
Page 183: type IIn Supernova SN 1995N,” 200
Page 190: and then can spiral in to the black
Page 195 and 196: Understanding the Evolution of Supe
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Radio  measurements  of  supe
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In the equations on the p
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SN 2008ax in NGC 4490 SN2008ax is a
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References Chevalier, R. A., “Int
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Computational Fluid Dynamical Model
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context of the k − ɛ model invol
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Figure 3: Experimental results (•
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direction results in the terminal s
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121 (2000). [Blue Ridge Numerics, I
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concentrated our effort specificall
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density, and Ps is a pressure tenso
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Properties of the GEM problem Recon
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Figure 1: Increase in reconnection
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Figure 3: Examples of agreement of
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Reflection and Refraction of Vortex
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Experimental Procedure The left han
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frames in the upper left corner, wh
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Vortex ring reflection. Similarly,
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References L Bernal and J Kwon. Vor
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group started in 1997 with the goal
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I conducted five semi-structured in
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In the example of the guinea pig pr
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explain t his t rend. F rom t alkin
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Research. Washington, DC: Pan Ameri
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Our team has two goals: 1. To put S
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fluctuating humidity, drying winds,
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western border of the Arkansas Rive
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adjusted to less than .4millisecond
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Cacti Experiment 18 has produced 10
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13. What N decomposer's are needed
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Abstract Toxic Offgassing Analysis
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The chambers were sealed and baked
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Tables 4 and 5 show offgassing comp
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there was no dichlorobenzene peak.
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eneficiation reagents. Ionic liquid
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Figure 3: Current versus voltage da
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Abstract New Initiatives in the Pro
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was noticed above the gel. A discol
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delicate structures (hairs). N o fu
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and A. Y. Rozanov, Eds., SPIE, Vol.
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Combining Writing Across the Curric
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But the study also reported a consi
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Educators’ Aerospace Workshop for
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2008-2009 Evaluation Educators’ A
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Some comments from participants 200
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The cost of a one credit graduate c
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EAA WOMEN SOAR - YOU SOAR Dr. Lee J
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� Incorporated the technology res
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Evaluation Results: At the conclusi
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Educational Standards: The National
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curriculum development, to provide
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and applications of GIS technology
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• A significant new outcome for t
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The design of this project and appl
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Activities at the workshop involved
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to give our students a series of PR
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In the past we have not focused on
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Providing High School Students with
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that th e current generations of s
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instruction a s pa rt o f t heir ow
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Wisconsin Space Grant Consortium &
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11:45-1:00 pm Lunch *** Concurrent
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Moderator: David B lock, A ssociate
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Second Place, E ngineering, Drew an
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Wisconsin Space Grant Consortium
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Space Grant Consortium - University of Wisconsin - Green Bay

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