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The Theme Park As "De Sprookjessprokkelaar," the Gatherer and Teller of Stories
University of Central Florida STARS Electronic Theses and Dissertations, 2004-2019 2018 Exploring a Three-Dimensional Narrative Medium: The Theme Park as "De Sprookjessprokkelaar," The Gatherer and Teller of Stories Carissa Baker University of Central Florida, [email protected] Part of the Rhetoric Commons, and the Tourism and Travel Commons Find similar works at: https://stars.library.ucf.edu/etd University of Central Florida Libraries http://library.ucf.edu This Doctoral Dissertation (Open Access) is brought to you for free and open access by STARS. It has been accepted for inclusion in Electronic Theses and Dissertations, 2004-2019 by an authorized administrator of STARS. For more information, please contact [email protected]. STARS Citation Baker, Carissa, "Exploring a Three-Dimensional Narrative Medium: The Theme Park as "De Sprookjessprokkelaar," The Gatherer and Teller of Stories" (2018). Electronic Theses and Dissertations, 2004-2019. 5795. https://stars.library.ucf.edu/etd/5795 EXPLORING A THREE-DIMENSIONAL NARRATIVE MEDIUM: THE THEME PARK AS “DE SPROOKJESSPROKKELAAR,” THE GATHERER AND TELLER OF STORIES by CARISSA ANN BAKER B.A. Chapman University, 2006 M.A. University of Central Florida, 2008 A dissertation submitted in partial fulfillment of the requirements for the degree of Doctor of Philosophy in the College of Arts and Humanities at the University of Central Florida Orlando, FL Spring Term 2018 Major Professor: Rudy McDaniel © 2018 Carissa Ann Baker ii ABSTRACT This dissertation examines the pervasiveness of storytelling in theme parks and establishes the theme park as a distinct narrative medium. It traces the characteristics of theme park storytelling, how it has changed over time, and what makes the medium unique. -
2020 FLOAT JUDGES BIOS Hitomi Gilliam AIFD Is a Japanese
2020 FLOAT JUDGES BIOS Hitomi Gilliam AIFD is a Japanese Canadian flower artist and has guest-designed throughout North America, England, Northern Ireland, Japan, Mexico, Taiwan, Bermuda, Singapore, Hong Kong, Australia, New Zealand, Colombia, Belgium, Korea, Costa Rica, India and Oman. Hitomi was one of five commissioned inter-disciplinary artists to show her floral art installation ‘RISE’ at ‘Les Fleurs Sauvages’ Art Show at Sotheby’s Institute of Art in New York City. Hitomi is Founder of the Annual ‘Survival of the Creative Minds’ Conference in Taos, New Mexico. 20th Annual Conference ‘REFLECTION’ is scheduled for October 2019. She is the founder of ‘Trend Summit’, a biennial conference – 5th edition is scheduled for March 2020 in Vancouver, Canada. Hitomi has lectured at Art Gallery of Ontario (Toronto), Chicago Botanical Gardens, Philadelphia Museum of Art, Cheekwood Botanical Gardens (Nashville), Museum of Fine Art Boston, Minneapolis Institute of Art, Bouquets to Art at DeYoung Museum (San Francisco), Houston Museum of Fine Art, New Orleans Museum of Fine Art, Cleveland Botanical Gardens, Honolulu Academy of Art, Everson Museum of Art (Syracuse), The Walters Art Museum (Baltimore), Longwood Gardens, Virginia Museum of Fine Art, Lewis Ginter Botanical Gardens (Richmond,VA), Detroit Institute of Arts, Vero Beach Museum of Fine Arts, The Strong Museum (Rochester, NY), North Carolina Museum of Art (Raleigh, NC) and Columbus Museum of Fine Art. She has presented at the Philadelphia Flower Show, Newport Flower Show and Singapore Garden Festival. Hitomi began her career in the Green Profession as a farmer/florist. She currently works with her son, Colin Gilliam in an Event & Education business, DESIGN358. -
Breakthrough Propulsion Study Assessing Interstellar Flight Challenges and Prospects
Breakthrough Propulsion Study Assessing Interstellar Flight Challenges and Prospects NASA Grant No. NNX17AE81G First Year Report Prepared by: Marc G. Millis, Jeff Greason, Rhonda Stevenson Tau Zero Foundation Business Office: 1053 East Third Avenue Broomfield, CO 80020 Prepared for: NASA Headquarters, Space Technology Mission Directorate (STMD) and NASA Innovative Advanced Concepts (NIAC) Washington, DC 20546 June 2018 Millis 2018 Grant NNX17AE81G_for_CR.docx pg 1 of 69 ABSTRACT Progress toward developing an evaluation process for interstellar propulsion and power options is described. The goal is to contrast the challenges, mission choices, and emerging prospects for propulsion and power, to identify which prospects might be more advantageous and under what circumstances, and to identify which technology details might have greater impacts. Unlike prior studies, the infrastructure expenses and prospects for breakthrough advances are included. This first year's focus is on determining the key questions to enable the analysis. Accordingly, a work breakdown structure to organize the information and associated list of variables is offered. A flow diagram of the basic analysis is presented, as well as more detailed methods to convert the performance measures of disparate propulsion methods into common measures of energy, mass, time, and power. Other methods for equitable comparisons include evaluating the prospects under the same assumptions of payload, mission trajectory, and available energy. Missions are divided into three eras of readiness (precursors, era of infrastructure, and era of breakthroughs) as a first step before proceeding to include comparisons of technology advancement rates. Final evaluation "figures of merit" are offered. Preliminary lists of mission architectures and propulsion prospects are provided. -
Theory of Space Magnetic Sail Some Common Mistakes and Electrostatic Magsail
1 Article MagSail after Cath for J 10 1 6 06 AIAA -2006 -8148 Theory of Space Magnetic Sail Some Common Mistakes and Electrostatic MagSail * Alexander Bolonkin C&R, 1310 Avenue R, #F -6, Brooklyn, NY 11229, USA T/F 718 -339 -4563, [email protected], http://Bolonki n.narod.ru Abstract The first reports on the “Space Magnetic Sail” concept appeared more 30 years ago. During the period since some hundreds of research and scientific works have been published, including hundreds of research report by professors at major famous universities. The author herein shows that all these works related to Space Magnetic Sail concept are technically incorrect because their authors did not take into consideration that solar wind impinging a MagSail magnetic field creates a particle m agnetic field opposed to the MagSail field. In the incorrect works, the particle magnetic field is hundreds times stronger than a MagSail magnetic field. That means all the laborious and costly computations in revealed in such technology discussions are us eless: the impractical findings on sail thrust (drag), time of flight within the Solar System and speed of interstellar trips are essentially worthless working data! The author reveals the correct equations for any estimated performance of a Magnetic Sail as well as a new type of Magnetic Sail (without a matter ring). Key words: magnetic sail, theory of MagSail, space magnetic sail, Electrostatic MagSail *Presented to 14th AIAA/AHI Space Planes and Hypersonic Systems and Technologies Conference , 6 - 9 Nov 2006 National Convention Centre, Canberra, Australia. Introduction The idea of utilizing the magnetic field to aggregate matter in space, harnessing a drag from solar wind or receiving a thrust from an Earth - charged particle beam is old. -
9.0 BACKGROUND “What Do I Do First?” You Need to Research a Card (Thruster Or 9.1 DESIGNER’S NOTES Robonaut) with a Low Fuel Consumption
9.2 TIPS FOR INEXPERIENCED ROCKET CADETS 9.0 BACKGROUND “What do I do first?” You need to research a card (thruster or 9.1 DESIGNER’S NOTES robonaut) with a low fuel consumption. A “1” is great, a “4” The original concept for this game was a “Lords of the Sierra Madre” in is marginal. The PRC player*** can consider an dash to space. With mines, ranches, smelters, and rail lines all purchased and claim Hellas Basin on Mars, using just his crew card. He controlled by different players, who have to negotiate between them- needs 19 fuel steps (6 WT) along the red route to do this. selves to expand. But space does not work this way. “What does my rocket need?” Your rocket needs 4 things: Suppose you have a smelter on one main-belt asteroid, powered by a • A card with a thruster triangle (2.4D) to act as a thruster. • A card with an ISRU rating, if its mission is to prospect. beam-station on another asteroid, and you discover platinum on a third • A refinery, if its mission is to build a factory. nearby asteroid. Unfortunately for long-term operations, next year these • Enough fuel to get to the destination. asteroids will be separated by 2 to 6 AUs.* Furthermore, main belt Decide between a small rocket able to make multiple claims, Hohmann transfers are about 2 years long, with optimal transfer opportu- or a big rocket including a refinery and robonaut able to nities about 7 years apart. Jerry Pournelle in his book “A Step Farther industrialize the first successful claim. -
The Hettema Group Celebrates 15 Years
The Hettema Group #70 • volume 13, issue 5 • 2017 www.inparkmagazine.com celebrates 15 years I-Drive 360 Serving up servers IAAPA overload Surviving and thriving in the Media based attractions All the latest and greatest our shadow of theme park giants depend on them industry has to offer 1 inparkmagazine.com inparkmagazine.com 2 inparkmagazine.com inparkmagazine.com Gold Sponsor2017 We Take Fun Seriously! Audio Video Projection Lighting Control Engineering Design Installation UAE - Germany - Finland - UK - Japan - Italy - China - USA 4 www.wartsila.com/funa inparkmagazine.com Anniversaries abound Immersion and IP Martin Palicki, Judith Rubin, IPM publisher IPM editor he IAAPA Expo has always been a big party in eople want to be immersed in stories and Tmany ways, but this year the celebrations seem Pincreasingly, the latest tech allows us to do that even more special. As we’ve put together this issue seamlessly. That seems to be what is demanded by (our 70th issue, wrapping up lucky year number 13), we today’s IP-centric media-based experiences realized many companies are celebrating milestones. What are the benefits of immersion? Guests stay From the 15th anniversary of our cover story longer, forget the day-to day-world, are emotionally company, The Hettema Group, to Sally Corporation’s engaged, spend more money and return more often. 40th birthday, there are success stories for companies Immersion is a product, somewhat intangible. Success of all sizes. is in the results. Immersion maintains the bubble of the experience. Is that a physical thing? A technological This is good news for all of us. -
Magnetoshell Aerocapture: Advances Toward Concept Feasibility
Magnetoshell Aerocapture: Advances Toward Concept Feasibility Charles L. Kelly A thesis submitted in partial fulfillment of the requirements for the degree of Master of Science in Aeronautics & Astronautics University of Washington 2018 Committee: Uri Shumlak, Chair Justin Little Program Authorized to Offer Degree: Aeronautics & Astronautics c Copyright 2018 Charles L. Kelly University of Washington Abstract Magnetoshell Aerocapture: Advances Toward Concept Feasibility Charles L. Kelly Chair of the Supervisory Committee: Professor Uri Shumlak Aeronautics & Astronautics Magnetoshell Aerocapture (MAC) is a novel technology that proposes to use drag on a dipole plasma in planetary atmospheres as an orbit insertion technique. It aims to augment the benefits of traditional aerocapture by trapping particles over a much larger area than physical structures can reach. This enables aerocapture at higher altitudes, greatly reducing the heat load and dynamic pressure on spacecraft surfaces. The technology is in its early stages of development, and has yet to demonstrate feasibility in an orbit-representative envi- ronment. The lack of a proof-of-concept stems mainly from the unavailability of large-scale, high-velocity test facilities that can accurately simulate the aerocapture environment. In this thesis, several avenues are identified that can bring MAC closer to a successful demonstration of concept feasibility. A custom orbit code that dynamically couples magnetoshell physics with trajectory prop- agation is developed and benchmarked. The code is used to simulate MAC maneuvers for a 60 ton payload at Mars and a 1 ton payload at Neptune, both proposed NASA mis- sions that are not possible with modern flight-ready technology. In both simulations, MAC successfully completes the maneuver and is shown to produce low dynamic pressures and continuously-variable drag characteristics. -
Future Space Transportation Technology: Prospects and Priorities
Future Space Transportation Technology: Prospects and Priorities David Harris Projects Integration Manager Matt Bille and Lisa Reed In-Space Propulsion Technology Projects Office Booz Allen Hamilton Marshall Space Flight Center 12 1 S. Tejon, Suite 900 MSFC, AL 35812 Colorado Springs, CO 80903 [email protected] [email protected] / [email protected] ABSTRACT. The Transportation Working Group (TWG) was chartered by the NASA Exploration Team (NEXT) to conceptualize, define, and advocate within NASA the space transportation architectures and technologies required to enable the human and robotic exploration and development of‘ space envisioned by the NEXT. In 2002, the NEXT tasked the TWG to assess exploration space transportation requirements versus current and prospective Earth-to-Orbit (ETO) and in-space transportation systems, technologies, and rcsearch, in order to identify investment gaps and recommend priorities. The result was a study nom’ being incorporatcd into future planning by the NASA Space Architect and supporting organizations. This papcr documents the process used to identify exploration space transportation investment gaps ;IS well as tlie group’s recommendations for closing these gaps and prioritizing areas of future investment for NASA work on advanced propulsion systems. Introduction investments needed to close gaps before the point of flight demonstration or test. The NASA Exploration Team (NEXT) was chartered to: Achieving robotic, and eventually, human presence beyond low Earth orbit (LEO) will Create and maintain a long-term require an agency-wide commitment of NASA strategic vision lor science-driven centers working together as “one NASA.” humanhobotic exploration Propulsion technology advancements are vital if NASA is to extend a human presence beyond the Conduct advanced concepts analym Earth’s neighhorhood. -
Cislunar Tether Transport System
FINAL REPORT on NIAC Phase I Contract 07600-011 with NASA Institute for Advanced Concepts, Universities Space Research Association CISLUNAR TETHER TRANSPORT SYSTEM Report submitted by: TETHERS UNLIMITED, INC. 8114 Pebble Ct., Clinton WA 98236-9240 Phone: (206) 306-0400 Fax: -0537 email: [email protected] www.tethers.com Report dated: May 30, 1999 Period of Performance: November 1, 1998 to April 30, 1999 PROJECT SUMMARY PHASE I CONTRACT NUMBER NIAC-07600-011 TITLE OF PROJECT CISLUNAR TETHER TRANSPORT SYSTEM NAME AND ADDRESS OF PERFORMING ORGANIZATION (Firm Name, Mail Address, City/State/Zip Tethers Unlimited, Inc. 8114 Pebble Ct., Clinton WA 98236-9240 [email protected] PRINCIPAL INVESTIGATOR Robert P. Hoyt, Ph.D. ABSTRACT The Phase I effort developed a design for a space systems architecture for repeatedly transporting payloads between low Earth orbit and the surface of the moon without significant use of propellant. This architecture consists of one rotating tether in elliptical, equatorial Earth orbit and a second rotating tether in a circular low lunar orbit. The Earth-orbit tether picks up a payload from a circular low Earth orbit and tosses it into a minimal-energy lunar transfer orbit. When the payload arrives at the Moon, the lunar tether catches it and deposits it on the surface of the Moon. Simultaneously, the lunar tether picks up a lunar payload to be sent down to the Earth orbit tether. By transporting equal masses to and from the Moon, the orbital energy and momentum of the system can be conserved, eliminating the need for transfer propellant. Using currently available high-strength tether materials, this system could be built with a total mass of less than 28 times the mass of the payloads it can transport. -
Title Study on Propulsive Characteristics of Magnetic Sail And
Study on Propulsive Characteristics of Magnetic Sail and Title Magneto Plasma Sail by Plasma Particle Simulations( Dissertation_全文 ) Author(s) Ashida, Yasumasa Citation 京都大学 Issue Date 2014-01-23 URL https://doi.org/10.14989/doctor.k17984 Right Type Thesis or Dissertation Textversion ETD Kyoto University Acknowledgment I would like to acknowledge many people supporting my doctorate study. My supervisor, Professor Hiroshi Yamakawa of Research Institute for Sustainable Humanosphere (RISH) of Kyoto University, supported my research throughout my master’s and doctor’s course. His valuable suggestions and advises indicated the guideline of my study, and especially, I learned the attitude toward researches. In addition, his work as the member of Strategic Headquarters for Space Policy has aroused my enthusiasm about the further evolution of the space exploration industry and a desire to contribute to it. I am deeply grateful for him. I am most grateful to Associate Professor Ikkoh Funaki of The Institute of Space and Astro- nautical Science (ISAS) of Japan Aerospace Exploration Agency (JAXA) for his advice. I am thankful for giving me a chance to start the study on the propulsion system making use of the solar wind. He had helped me since the beginning of my study. I would like to express my deep gratitude to him. I want to thank Associate Professor Hirotsugu Kojima of RISH/Kyoto University. He taught me various knowledge about plasma physics, the experimental studies and so on. I greatly appreciate Professor Tetsuji Matsuo of Kyoto University for our fruitful discussions and for reviewing this thesis. I also sincerely thank him for his many helpful comments and astute suggestions. -
Creating an Inclusive Community
Spring 2018 l No. 39 No. Sergio Rebia leads a drawing demonstration on Application Day at Cal State Fullerton. 51 students from 45 high schools attended, and 75% of them later applied to Ryman Arts Creating an Inclusive Community “I encourage my students to apply [to Ryman Arts] because it forces them out of their bubble of comfort and complacency. Students are exposed to quality art supplies and instruction they may not be able to afford on their own,” says L’lia Thomas (Ms. T) from La Tijera K-8 Academy of Excellence Charter School. Every year, Ryman Arts connects with over 2,000 Ms. T is an exemplary model of the community students through school presentations, community champions we count on to learn about student fairs, and Application Days. These efforts combat needs in our communities. Because of her the challenges that some students experience in initiative, we have continued to build our learning about and completing the application to relationship with La Tijera Charter School and Ms. T (second from left) and students from La Tijera our highly competitive program. Through strong recently added a special in-school workshop for Charter School relationships with public school teachers like her students. Ms. T, we have made great strides in “It was incredible having Miss Robin come out increasing access to Ryman Arts. to my classroom to facilitate a two-day workshop Application Days have been successful for students who are applying. Her approach in in creating a supportive environment my classroom gave students a real taste of what it where prospective students can take an would be like [at Ryman Arts].” introductory drawing class led by one of Ensuring broad access to Ryman Arts remains our faculty and work on a still life that an important part of our efforts because of the can be included in their application. -
Remembering World War Ii in the Late 1990S
REMEMBERING WORLD WAR II IN THE LATE 1990S: A CASE OF PROSTHETIC MEMORY By JONATHAN MONROE BULLINGER A dissertation submitted to the Graduate School-New Brunswick Rutgers, The State University of New Jersey In partial fulfillment of the requirements For the degree of Doctor of Philosophy Graduate Program in Communication, Information, and Library Studies Written under the direction of Dr. Susan Keith and approved by Dr. Melissa Aronczyk ________________________________________ Dr. Jack Bratich _____________________________________________ Dr. Susan Keith ______________________________________________ Dr. Yael Zerubavel ___________________________________________ New Brunswick, New Jersey January 2017 ABSTRACT OF THE DISSERTATION Remembering World War II in the Late 1990s: A Case of Prosthetic Memory JONATHAN MONROE BULLINGER Dissertation Director: Dr. Susan Keith This dissertation analyzes the late 1990s US remembrance of World War II utilizing Alison Landsberg’s (2004) concept of prosthetic memory. Building upon previous scholarship regarding World War II and memory (Beidler, 1998; Wood, 2006; Bodnar, 2010; Ramsay, 2015), this dissertation analyzes key works including Saving Private Ryan (1998), The Greatest Generation (1998), The Thin Red Line (1998), Medal of Honor (1999), Band of Brothers (2001), Call of Duty (2003), and The Pacific (2010) in order to better understand the version of World War II promulgated by Stephen E. Ambrose, Tom Brokaw, Steven Spielberg, and Tom Hanks. Arguing that this time period and its World War II representations