Space Grant Consortium - University of Wisconsin - Green Bay

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Wisconsin Space Grant Consortium Undergraduate Scholarship Program Supports outstanding undergraduate students pursuing aerospace, space science, or other space-related studies or research. Undergraduate Research Awards Supports qualifi ed students to create and implement a small research study of their own design during the summer or academic year that is directly related to their interests and career objectives in space science, aerospace, or space-related studies. Graduate Fellowships Support outstanding graduate students pursuing aerospace, space science, or other interdisciplinary space-related graduate research. Dr. Laurel Salton Clark Memorial Graduate Fellowship In honor of Dr. Clark, Columbia Space Shuttle astronaut and resident of Wisconsin, this award supports a graduate student pursuing studies in the fi elds of environmental or life sciences, whose research has an aerospace component. University Sounding Rocket Team Competition Provides an opportunity and funding for student teams to design and fl y a rocket that excels at a specifi c goal that is changed annually. High School Sounding Rocket Team Competition For high school students. This program is in its initial stages. It mimics the university competition. Student High-Altitude Balloon Instrument Development Students participate in this instrument development program through engineering or science teams. Working models created by the students will be fl own on high-altitude balloons. Student Programs for 2009 vi Student High-Altitude Balloon Payload/ Launch Program The Elijah Project is a high-altitude balloon program in which science and engineering students work in integrated science and engineering teams, to design, construct, launch, recover and analyze data from a high-altitude balloon payload. These balloons travel up to 100,000 ft., considered “the edge of space.” Selected students will join either a launch team or a payload design team. Industry Member Internships Supports student internships in space science or engineering for the summer or academic year at WSGC Industry members co-sponsored by WSGC and Industry partners. NASA ESMD Internships Supports student internships at NASA centers or WSGC industry members that tie into NASA’s Exploration Systems Mission Directorates. NASA Academy Leadership Internships This summer internship program at NASA Centers promotes leadership internships for college juniors, seniors and fi rst-year graduate students and is co-sponsored by participating state Space Grant Consortia. NASA Centers/JPL Internships Supports WSGC students for research internships at NASA Centers or JPL. NASA Reduced Gravity Program Operated by the NASA Johnson Space Center, this program provides the unique “weightless” environment of space fl ight for test and training purposes. WSGC student teams submit reduced gravity experiments to NASA and, if selected, get to perform their experiments during a weightless environment fl ight with the support of WSGC. Relevant Student Travel Supports student travel to present their WSGC-funded research.
Preface 19th Annual Conference TABLE OF CONTENTS Part 1: Student Satellite Program: High Altitude Balloon Balloon Launch Team: Eric Deering, Milwaukee School of Engineering Brian Nguyen, Milwaukee School of Engineering Nathan Sward, 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 Part 2: Student Satellite Program: Rocket Design Competition 1 st Place – Non Engineering Schmitt Triggers Brad Hartl, University of Wisconsin-La Crosse Jacob Wardon, University of Wisconsin-La Crosse Steven Welter, Western Technical College Mark Witte, University of Wisconsin-La Crosse 1 st Place – Engineering Team Narwhal, Milwaukee School of Engineering Neal Bitter, Team Leader Adam Harden Chelsey Jelinski 2 nd Place - Engineering Team Drew and Crew - Milwaukee School of Engineering Drew Falkenburg, Team Leader Wes Larrabee Caleb Varner 3rd Place - Engineering Rocky Mountain Miners - Milwaukee School of Engineering Brian Mortensen, Team Leader Ryan May Jon Neujahr vii
Page 1 and 2: Space Grant Consortium wisconsin UN
Page 3 and 4: THE CASSINI ENCOUNTER WITH THE GEM
Page 5: Th he proceedinngs of our 199th Ann
Page 10 and 11: Part 3: NASA Reduced Gravity Progra
Page 12 and 13: EAA Women Soar - You Soar, Lee Siud
Page 15 and 16: Elijah High Altitude Balloon Projec
Page 17 and 18: Our experience with the HALO II lau
Page 19 and 20: which had been a problem in the pas
Page 21: Figure 6: 3-D GPS Generated Track o
Page 24 and 25: Results The seeds tested in the lab
Page 26 and 27: hour as we assumed the flight in th
Page 28 and 29: Experimental Results There are two
Page 30 and 31: A series of tests were done in a co
Page 32 and 33: 380 360 340 320 23.3 Temp. (Celsius
Page 35 and 36: First Place, Non-Engineering: Schmi
Page 37 and 38: of the basis for fin designs came f
Page 39 and 40: ejection charge from the motor fire
Page 41 and 42: using rip-stop nylon cloth. To atta
Page 43 and 44: Post-flight recovery. A field searc
Page 45 and 46: Thus, it is believed that the main
Page 47: [2] Public Missiles Ltd. Frequently
Page 50 and 51: Design Features The chief requireme
Page 52 and 53: The joint between the dart and the
Page 54 and 55: Area dramatically influenced by flo
Page 56 and 57: 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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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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