Space Grant Consortium - University of Wisconsin - Green Bay

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Wisconsin Space Conference Friday, August 15, 2008 8:00-9:00 am Registration Todd Wehr Conference Center Breakfast 8:00-8:45 am Undergraduate Workshop CC130 *** Plenary Session *** 9:00-10:00 am Session 5: Keynote Address Todd Wehr Conference Center Dr. Ellis Miner, The Cassini Encounter with the Gem of the Solar System II, NASA Science Manager for the Cassini Mission to Saturn 10:00-10:30 am Morning Break and Refreshments 10:30-12:00 am Session 6: Student Satellite Program *** Plenary Session *** Moderator: Bill Farrow, WSGC Associate Director for Special Initiatives, Assistant Professor, Milwaukee School of Engineering Balloon Payload Team: Antonio Castillo, University of Wisconsin-Madison Brittany Hauser, Milwaukee School of Engineering Zachary Parsons, Milwaukee School of Engineering Chris Reichard, Milwaukee School of Engineering Victorialynn Salas, Marquette University Max Witte, Milwaukee School of Engineering Balloon Launch Team: Eric Deering, Milwaukee School of Engineering Brian Nguyen, Milwaukee School of Engineering Nathan Sward, Milwaukee School of Engineering Sounding Rocket Teams: First P lace, N on-Engineering, Schmitt Triggers, Brad H artl r epresenting t eam members: J acob W ardon, S teven W elter, M ark W itte, U W-LaCrosse and W estern Technical College 6
Second Place, E ngineering, Drew and Crew, Wesley L arrabee representing t eam members D rew Falkenburg, C aleb V arner, Undergraduates, M ilwaukee S chool of Engineering 12:00-12:15 pm Group Photograph As Directed 12:15-1:15 pm Awards Luncheon Todd Wehr Conference Center 1:15-1:45 pm Awards Ceremony R. Aileen Yingst, Director, Wisconsin Space Grant Consortium Sharon D. Brandt, Program Manager, Wisconsin Space Grant Consortium Karen Valley, Chair, WSGC Advisory Council Program Associate Directors 1:45-2:00 pm 2010 Conference 2:00 pm Conference Adjourned *** Adjournment *** 2:00-4:00 pm Advanced Undergraduate Research Workshop Computer Lab, S-130 7
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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
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Figure 2: Screen I mage o f G UI. T
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References ¹ Burnham, D.C., and Ha
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Validation of Novel Rigid Body Fric
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forces is implemented in the popula
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Figure 2. CAD representation of a t
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Results Figure 5. Assembled hydraul
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References Anitescu, M. (2006). "Op
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Multi-stage Joule-Thomson cycles ar
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significant change in total compres
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The enthalpy (h3) of the 2 nd stage
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UA m� ⎛ ε −1 ⎞ ( c nd c st
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educed, the temperature range that
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7. Lemmon, E. W.; Huber, M. L.; McL
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Throughout each of the run cycles,
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and heater adjusted to accommodate
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Phaeton Mast Dynamics Mechanical Sy
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exposure to the FEMAP with NASTRAN
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The irregularity in the plots above
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inversion of a particular matrix, t
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clarified. Additionally, the PMD ki
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A. Abstract For hardware to be flig
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should be performed at the JWST obs
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B. Attenuation and Uncertainty Shoc
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Detector Array and ROIC SCA Mount L
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Detector Shock Environment The leve
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Orbiter (MRO), Moon Mineralogy Mapp
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4. NASA JPL. MIRI FOCAL PLANE SYSTE
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Is Lake Superior a significant sour
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each grid cell at daily resolution.
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Figure 3. (a) Seasonal cycle of lak
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Figure 5. Model pCO2 at the surface
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Marshall, J., A. Adcroft, C. Hill,
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numerical weather prediction (NWP)
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High Resolution Radiometer (AVHRR)
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On the morning of 26 May 2008, ther
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References Behnke, C., 2005: Synopt
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Figure 3 Figure 3 contains base ref
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A Comparative Study of Type IIb Sup
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Fig. 3.— Cartoon Image of SN blas
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Fig. 4.— Light curve of SN 2008bo
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type IIn Supernova SN 1995N,” 200
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and then can spiral in to the black
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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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Page 291 and 292: But the study also reported a consi
Page 293 and 294: Educators’ Aerospace Workshop for
Page 295 and 296: 2008-2009 Evaluation Educators’ A
Page 297: Some comments from participants 200
Page 300 and 301: The cost of a one credit graduate c
Page 303: EAA WOMEN SOAR - YOU SOAR Dr. Lee J
Page 306 and 307: � Incorporated the technology res
Page 308 and 309: Evaluation Results: At the conclusi
Page 310 and 311: Educational Standards: The National
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Page 335 and 336: Wisconsin Space Grant Consortium &
Page 337 and 338: 11:45-1:00 pm Lunch *** Concurrent
Page 339: Moderator: David B lock, A ssociate
Page 343: Wisconsin Space Grant Consortium
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Space Grant Consortium - University of Wisconsin - Green Bay

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