Space Grant Consortium - University of Wisconsin - Green Bay

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Activities and labs were provided by many sources. Specific activities and providers: Hot Wheels –It’s A Drag activity, Mattel [and J. Blake/self-developed]; Outer Space Chemistry, Fire Arrows Kit, SK/ Boreal Labs; Living on the Shuttle, Lunar Survival Test, NASA Inquiry Stations, Toys in Space, NASA; Fuel Cell Challenge, [J. Blake/self-developed]; C.O.G.bottle activity, Arizona Aerospach Outreach; Microgravity Demo/Bottles,[J. Blake/self-developed; Space Station Magna, AIMS [and J. Blake/self-developed]; Mars Mission/miscellaneous materials, Evan Moore Corp. and Aerospace Education Services Project-Oklahoma State University; Shuttle & Orbiter outline sketches & associated drawings/miscellaneous activities, Wisconsin Aviation Careers – Wisconsin DOT, Bureau of Aeronautics. Science lab materials housed in the science lab at Brookwood Middle School, consumables like paper, glue, string, etc. as well as small hand tools, and so forth were made available, as needed. Evaluation. At the end of each session, participants were asked to respond to an evaluation form. It consisted of seven parts. The first five statements required a ranking of the individual statement, one to five. A rank of five indicated a strongly agree (SA) response while a rank of one indicated a strongly disagree (SD) response. The sixth statement listed several activities using nine capital letters, A through H. Participants were asked to circle the letters of the activities they enjoyed the most with the understanding that they could circle all letters, if desired. The seventh statement allowed the teachers a chance to write any additional comments about the workshop. The results of this evaluation, including comments from participants can be found in pages that follow. An instructor’s journal was kept regarding each Saturday session. Reflecting on what went well, what needed more in-depth explanation or coverage and what could have been done better was the purpose of the journal. Further study of these notes, immediately following each session, served to help improve any future workshops presented related to aerospace and flight. References – cited in last paragraph, Program Focus AIMS & self [Jack Blake] Space Station Magna Arizona Aerospace Outreach C.O.G. Evan Moore Corp. & Aerospace Education Services-OSU Mars mission/miscellaneous activities Mattel Toys & self [Jack Blake] HotWheels-It’s A Drag Activity NASA, Living on the Shuttle, Lunar Survival Test, NASA Inquiry Stations, Toys in Space Science Kit and Boreal Labs Outer Space Chemistry, Fire Arrows Self [Jack Blake] Fuel Cell, Microgravity Demo/Bottle Wisconsin DOT, Bureau of Aeronautics Shuttle & Orbiter sketch/miscellaneous activities 6
2008-2009 Evaluation Educators’ Aerospace Workshop for the 21 st Century Please circle the correct number for the statements below by using the following scale: 5 = Strongly Agree 4=Agree 3=Uncertain 2=Disagree 1=Strongly Disagree The Workshop: SA A U D SD 1) Increased my knowledge about aviation, 5 4 3 2 1 aerospace concepts and principles. 2) Increased my interest in this subject. 5 4 3 2 1 3) Increased my confidence in doing science 5 4 3 2 1 activities. 4) Provided me the opportunity to interact and 5 4 3 2 1 work in cooperative groups. 5) Provided many hands-on aerospace activities. 5 4 3 2 1 6) Which of the following activities did you enjoy the most? {Please circle as many letters as you would like} A. Microgravity Demo/Bottles B. Toys in Space C. Lunar Survival Test D. NASA Inquiry Stations E. Fire Arrows/Rockets F. Fuel Cell challenge G. HotWheels-It’s A Drag H. Outer Space Chemistry I. C.O.G. 7) On the back of this form, please write any additional comments about things you liked or disliked about the workshop. 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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Page 300 and 301: The cost of a one credit graduate c
Page 303: EAA WOMEN SOAR - YOU SOAR Dr. Lee J
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Page 308 and 309: Evaluation Results: At the conclusi
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Space Grant Consortium - University of Wisconsin - Green Bay

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