Space Station Freedom. a Foothold on the Future. INSTITUTION National Aeronautics and Space Administration, Washington, DC
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The Journey to Mars: How Donna Shirley Broke Barriers for Women in Space Engineering
The Journey to Mars: How Donna Shirley Broke Barriers for Women in Space Engineering Laurel Mossman, Kate Schein, and Amelia Peoples Senior Division Group Documentary Word Count: 499 Our group chose the topic, Donna Shirley and her Mars rover, because of our connections and our interest level in not only science but strong, determined women. One of our group member’s mothers worked for a man under Ms. Shirley when she was developing the Mars rover. This provided us with a connection to Ms. Shirley, which then gave us the amazing opportunity to interview her. In addition, our group is interested in the philosophy of equality and we have continuously created documentaries that revolve around this idea. Every member of our group is a female, so we understand the struggles and discrimination that women face in an everyday setting and wanted to share the story of a female that faced these struggles but overcame them. Thus after conducting a great amount of research, we fell in love with Donna Shirley’s story. Lastly, it was an added benefit that Ms. Shirley is from Oklahoma, making her story important to our state. All of these components made this topic extremely appealing to us. We conducted our research using online articles, Donna Shirley’s autobiography, “Managing Martians”, news coverage from the launch day, and our interview with Donna Shirley. We started our research process by reading Shirley’s autobiography. This gave us insight into her college life, her time working at the Jet Propulsion Laboratory, and what it was like being in charge of such a barrier-breaking mission. -
Solar Aircraft Design
Cumhuriyet Üniversitesi Fen Fakültesi Cumhuriyet University Faculty of Science Fen Bilimleri Dergisi (CFD), Cilt:36, No: 3 Özel Sayı (2015) Science Journal (CSJ), Vol. 36, No: 3 Special Issue (2015) ISSN: 1300-1949 ISSN: 1300-1949 SOLAR AIRCRAFT DESIGN Sadegh RAHMATI1,*, Amir GHASED2 1,2Department of Mechanical Engineering, Majlesi Branch, Islamic Azad University, Isfahan, Iran Received: 01.02.2015; Accepted: 05.05.2015 ______________________________________________________________________________________________ Abstract. Generally domain Aircraft uses conventional fuel. These fuel having limited life, high cost and pollutant. Also nowadays price of petrol and other fuels are going to be higher, because of scarcity of those fuels. So there is great demand of use of non-exhaustible unlimited source of energy like solar energy. Solar aircraft is one of the ways to utilize solar energy. Solar aircraft uses solar panel to collect the solar radiation for immediate use but it also store the remaining part for the night flight. This paper intended to stimulate research on renewable energy sources for aviation. In future solar powered air planes could be used for different types of aerial momitoring and unmanned flights. This review paper brietly shows history, application and use of solar aircraft. We are focusing on design and fabrication of solar aircraft which is unmanned prototype. Keywords: Solar energy, Reynolds number, Bernoulli’s principle 1. INTRODUCTION Energy comes in different forms. Light is a form of energy. Sun is source of energy called “sunlight”. Sunshine is free and never gets used up Also. There is a lot of it. The sunlight that heats the Earth in an hour has more energy than the people of the world use in a year. -
State of the Art of Piloted Electric Airplanes, NASA's Centennial Challenge Data and Fundamental Design Implications
Dissertations and Theses Fall 2011 State of the Art of Piloted Electric Airplanes, NASA's Centennial Challenge Data and Fundamental Design Implications Lori Anne Costello Embry-Riddle Aeronautical University - Daytona Beach Follow this and additional works at: https://commons.erau.edu/edt Part of the Aerospace Engineering Commons Scholarly Commons Citation Costello, Lori Anne, "State of the Art of Piloted Electric Airplanes, NASA's Centennial Challenge Data and Fundamental Design Implications" (2011). Dissertations and Theses. 37. https://commons.erau.edu/edt/37 This Thesis - Open Access is brought to you for free and open access by Scholarly Commons. It has been accepted for inclusion in Dissertations and Theses by an authorized administrator of Scholarly Commons. For more information, please contact [email protected]. STATE OF THE ART OF PILOTED ELECTRIC AIRPLANES, NASA’S CENTENNIAL CHALLENGE DATA AND FUNDAMENTAL DESIGN IMPLICATIONS by Lori Anne Costello A Thesis Submitted to the Graduate Studies Office in Partial Fulfillment of the Requirements for the Degree of Master of Science in Aerospace Engineering Embry-Riddle Aeronautical University Daytona Beach, Florida Fall 2011 1 Copyright by Lori Anne Costello 2011 All Rights Reserved 2 ACKNOWLEDGEMENTS This thesis is the culmination of two years of work on the Green Flight Challenge Eco-Eagle. The Eco- Eagle and this thesis would not have been possible without countless help and inspiration from friends and family. I would like to thank Dr. Anderson for giving me the opportunity to participate in Embry-Riddle’s Green Flight Challenge Team and for supporting me and the Eco-Eagle project. Without his guidance I would not have this paper and understood as much as I now do about electric airplanes. -
Paper Session III-B - Space Station On-Orbit Assembly and Operation
1991 (28th) Space Achievement: A Global The Space Congress® Proceedings Destiny Apr 25th, 1:00 PM - 4:00 PM Paper Session III-B - Space Station On-Orbit Assembly and Operation L. P. Morata Vice President, Deputy General Manager, McDonnell Douglas Space Systems Company, Huntington Beach CA F. David Riel Deputy Director, System Engineering and Integration, McDonnell Douglas Space Systems Company- Space Station Division Follow this and additional works at: https://commons.erau.edu/space-congress-proceedings Scholarly Commons Citation Morata, L. P. and Riel, F. David, "Paper Session III-B - Space Station On-Orbit Assembly and Operation" (1991). The Space Congress® Proceedings. 9. https://commons.erau.edu/space-congress-proceedings/proceedings-1991-28th/april-25-1991/9 This Event is brought to you for free and open access by the Conferences at Scholarly Commons. It has been accepted for inclusion in The Space Congress® Proceedings by an authorized administrator of Scholarly Commons. For more information, please contact [email protected]. SPACE STATION FREEDOM ASSEMBLY AND OPERATIONS Larry P. Morata Vice President, Deputy Project Manager—DDT&E McDonnell Douglas Space Systems Company-Space Station Division Huntington Beach, California and F. David Kiel Deputy Director, System. Engineering and Integration McDonnell Douglas Space Systems Company-Space Station Division Huntington Beach, California ABSTRACT Eight Man. Crew Capability (EMCC) by 31 December 2000 as shown, in Figure 1. The United States and its international partners are well Recent design, on the way to developing Space Station Freedom which will changes as part: of the SSF program restructure activity have be a very large orbiting facility with many capabilities for altered the Space Station configu ration and design from conducting space operations. -
Habitation Module 26 July 2016 – NASA Advisory Council, Human Exploration and Operations Committee
National Aeronautics and Space Administration Habitation Module 26 July 2016 – NASA Advisory Council, Human Exploration and Operations Committee Jason Crusan | Advanced Exploration Systems Director | NASA Headquarters 2 Human Exploration of Mars Is Hard Common Capability Needs Identified from Multiple Studies Days Reliable In-Space 800-1,100 44 min Transportation Total me crew is Maximum two- away from Earth – way communicaon for orbit missions all in 2me delay – 300 KW Micro-g and Radia2on Autonomous Opera2ons Total connuous transportaon power 130 t Heavy-LiA Mass 20-30 t Long Surface Stay Multiple Ability to 500 Days Launches per land large mission payloads Surface Operations Dust Toxicity and 100 km 11.2 km/s Long Range Explora2on Earth Entry Speed 20 t Oxygen produced for ascent to orbit - ISRU 3 The Habitation Development Challenge HABITATATION CAPABILITY Days 800-1,100 Habitation Systems – Total me crew is AES/ISS/STMD away from Earth – • Environmental Control & Life Support for orbit missions all in • Autonomous Systems Micro-g and Radia2on Integrated • EVA testing on ISS • Fire Safety • Radiation Protection Habitation Systems - Crew Health – HRP Long Surface Stay • Human Research 500 Days • Human Performance • Exercise PROVING GROUND Validation in cislunar space • Nutrition Habitation Capability– NextSTEP BAA / Int. Partners • Studies and ground prototypes of pressurized volumes 4 Specific Habitation Systems Objectives TODAY FUTURE Habitation The systems, tools, and protec:ons that allow Systems Elements humans to live and work -
Astronautics and Aeronautics: a Chronology, 1996-2000
ASTRONAUTICS AND AERONAUTICS: A CHRONOLOGY, 1996–2000 NASA SP-2009-4030 February 2009 Authors: Marieke Lewis and Ryan Swanson Project Manager: Alice R. Buchalter Federal Research Division, Library of Congress NASA History Division Office of External Relations NASA Headquarters Washington, DC 20546 Astronautics and Aeronautics: A Chronology, 1996-2000 PREFACE This report is a chronological compilation of narrative summaries of news reports and government documents highlighting significant events and developments in United States and foreign aeronautics and astronautics. It covers the years 1996 through 2000. These summaries provide a day-by-day recounting of major activities, such as administrative developments, awards, launches, scientific discoveries, corporate and government research results, and other events in countries with aeronautics and astronautics programs. Researchers used the archives and files housed in the NASA History Division, as well as reports and databases on the NASA Web site. i Astronautics and Aeronautics: A Chronology, 1996-2000 TABLE OF CONTENTS PREFACE........................................................................................................................................ i JANUARY 1996............................................................................................................................. 1 FEBRUARY 1996 .......................................................................................................................... 5 MARCH 1996................................................................................................................................ -
Internationale Raumstation ISS International Space Station ISS
Internationale Raumstation ISS International Space Station ISS www.DLR.de Europäisches Labormodul COLUMBUS European laboratory module COLUMBUS US-Labormodul DESTINY japanisches Labormodul KIBO US laboratory module DESTINY Japanese laboratory module KIBO Russisches Cargo-Modul SaRja (Functional Cargo Block) Russian cargo module ZARYA 20. November 1998: (Functional Cargo Block) 24. Februar 2011: Start des ersten ISS-Moduls: Start des permanenten der Functional Cargo Block Logistikmoduls PMM (FGB) Sarja Leonardo November 20, 1998: February 24, 2011: launch of the first ISS module: launch of the logistic the Functional Cargo Block module PMM Leonardo (FGB) Zarya 12. juli 2000: 8. Februar 2010: Start des Service- und Wohn- Start des Aussichtsmoduls moduls Swesda Cupola July 12, 2000: February 8, 2011: launch of the observatory launch of the service and Russisches Service-Modul habitation module Zvezda module Cupola SwESDa Russian service module 10. November 2009: 7. Februar 2001: Europäisches Logistikmodul aTV-2 Start des amerikanischen ZvEZDA Start des russischen Docking- Labormoduls DESTINY (automated Transfer Vehicle) moduls POISK Mini-Research „johannes Kepler“ Module 2 February 7, 2001: 7. Februar 2008: 31. Mai 2008: launch of the American European logistics module ATv-2 November 10, 2009: Start des europäischen Start des zweiten Teils des laboratory module DESTINY (Automated Transfer vehicle) launch of the Russian docking Labormoduls japanischen Labormoduls “Johannes Kepler” module POISK Mini-Research COLUMBUS KIBO Pressurized Module (PM) Module 2 February 7, 2008: May 31, 2008: launch of the European launch of the second part of the research module Japanese laboratory module KIBO COLUMBUS Pressurized Module (PM) ISS ISS © NASA, ESA, DLR Forschung im All für die Menschen auf der Erde Research in Space for Mankind on Earth. -
GUIDANCE, NAVIGATION, and CONTROL 2020 AAS PRESIDENT Carol S
GUIDANCE, NAVIGATION, AND CONTROL 2020 AAS PRESIDENT Carol S. Lane Cynergy LLC VICE PRESIDENT – PUBLICATIONS James V. McAdams KinetX Inc. EDITOR Jastesh Sud Lockheed Martin Space SERIES EDITOR Robert H. Jacobs Univelt, Incorporated Front Cover Illustration: Image: Checkpoint-Rehearsal-Movie-1024x720.gif Caption: “OSIRIS-REx Buzzes Sample Site Nightingale” Photo and Caption Credit: NASA/Goddard/University of Arizona Public Release Approval: Per multimedia guidelines from NASA Frontispiece Illustration: Image: NASA_Orion_EarthRise.jpg Caption: “Orion Primed for Deep Space Exploration” Photo Credit: NASA Public Release Approval: Per multimedia guidelines from NASA GUIDANCE, NAVIGATION, AND CONTROL 2020 Volume 172 ADVANCES IN THE ASTRONAUTICAL SCIENCES Edited by Jastesh Sud Proceedings of the 43rd AAS Rocky Mountain Section Guidance, Navigation and Control Conference held January 30 to February 5, 2020, Breckenridge, Colorado Published for the American Astronautical Society by Univelt, Incorporated, P.O. Box 28130, San Diego, California 92198 Web Site: http://www.univelt.com Copyright 2020 by AMERICAN ASTRONAUTICAL SOCIETY AAS Publications Office P.O. Box 28130 San Diego, California 92198 Affiliated with the American Association for the Advancement of Science Member of the International Astronautical Federation First Printing 2020 Library of Congress Card No. 57-43769 ISSN 0065-3438 ISBN 978-0-87703-669-2 (Hard Cover Plus CD ROM) ISBN 978-0-87703-670-8 (Digital Version) Published for the American Astronautical Society by Univelt, Incorporated, P.O. Box 28130, San Diego, California 92198 Web Site: http://www.univelt.com Printed and Bound in the U.S.A. FOREWORD HISTORICAL SUMMARY The annual American Astronautical Society Rocky Mountain Guidance, Navigation and Control Conference began as an informal exchange of ideas and reports of achievements among local guidance and control specialists. -
October 2011 Issue 2
Issue 2 October 2011 All about the Chinese Space Programme GO TAIKONAUTS! Editor’s Note As promised, this issue is delivered as a special issue on the Chinese space station Cover Story programme. The flawless launch of the Tiangong 1 was really ... page 2 Quarterly Report April - June 2011 Launch Events There were two success- ful space launches in the second quarter of 2011. On 10 April 2011 at 4:47:04 Beijing Time, a Long March 3A (Y19) lifted-off from Pad 3 in Xichang Satellite Launch Centre, putting the Beidou IGSO 3 navigation sat- ellite into orbit. It was the first Chinese Dawn of the Chinese Space Station Era space launch of 2011 and the eighth op- A Textbook Launch erational Beidou satellite. The satellite History turned a new page at 21:16:03 Beijing Time on 29 September 2011, entered its working orbit ... page 3 when a Long March 2F (CZ-2F T1) rocket lifted-off from Pad 921 at the Jiu- quan Satellite Launch Centre in China. In contrast with other launch vehicles that took-off from the same pad on previous occasions, ... page 6 Proposal Mutual Rescue Operations Between the On The Spot Tiangong and ISS? Background Touch the Chinese Space Programme in Three Days The ISS began six-crew member opera- Report from the 4th CSA-IAA Conference on Advanced Space Technology tion in 2009, and the U.S. shuttle retired in Shanghai in July 2011. Crew transportation and An Open and International Conference emergency rescue now totally depends To the Chinese space programme and people paying attention to it, early upon the Russian Soyuz vehicle. -
Orb2: Spherical Space Station Designed for Single Launch and On-Orbit Assembly
Orb2: Spherical Space Station Designed for Single Launch and On-Orbit Assembly Vojtech Holub ∗ Unaffiliated With upcoming heavy and super-heavy lift rockets targeted for launch in 2021, a new class of payloads can be launched into low Earth orbit. This paper presents a design for a space station capable of being lifted by a single Blue Origin New Glenn vehicle. Once assembled on-orbit, it contains more than twice the pressurized volume of the International Space Station. The pressurized volume of traditional space station modules is limited by the dimensions of the payload fairing. The proposed Orb2 design consists of a spherical habitation module and a service module. The habitation module avoids the volume limitation by being launched in a flat-packed stack and assembled and welded robotically in orbit. Using CAD and finite element analysis, this paper shows that the habitation module contains approximately 2000 m3 of pressurized volume, with a mass of 24 tons, and can hold four times the standard atmospheric pressure. Moreover, the Whipple shield configuration is identical to the heavily protected sections of the ISS. The service module has a traditional cylindrical design and its role is to provide all the necessary utilities. Furthermore, the paper explains the assembly and welding method required to convert Orb2 into the fully assembled space station. I. Nomenclature LEO = low Earth orbit ISS = International Space Station PAS = payload adapter system MMOD = micrometeoroids and orbital debris FEA = finite element analysis g = gravitational force, 9:81m/s2 EBW = electron beam welding BEAM = Bigelow Expandable Activity Module ∗Staff Research Engineer, Portland, OR, 97201 USA, Member AIAA. -
Effort to Accelerate MBSE Adoption and Usage at JSC
Effort to Accelerate MBSE Adoption and Usage at JSC Lui Wang1 NASA Johnson Space Center, Houston, TX 77058 and Michel Izygon, Ph.D.2, Shira Okon3, Larry Garner4, and Howard Wagner, Ph.D.5 Tietronix Software Inc., Houston, TX 77058 This paper describes the authors’ experience in adopting Model Based System Engineering (MBSE) at the NASA/Johnson Space Center (JSC). Since 2009, NASA/JSC has been applying MBSE using the Systems Modeling Language (SysML) to a number of advanced projects. Models integrate views of the system from multiple perspectives, capturing the system design information for multiple stakeholders. This method has allowed engineers to better control changes, improve traceability from requirements to design and manage the numerous interactions between components. As the project progresses, the models become the official source of information and used by multiple stakeholders. Three major types of challenges that hamper the adoption of the MBSE technology are described. These challenges are addressed by a multipronged approach that includes educating the main stakeholders, implementing an organizational infrastructure that supports the adoption effort, defining a set of modeling guidelines to help engineers in their modeling effort, providing a toolset that support the generation of valuable products, and providing a library of reusable models. JSC project case studies are presented to illustrate how the proposed approach has been successfully applied. Nomenclature CAD = Computer-Aided Design CDS = Cascade Distillation System -
Closing Comments
Closing Comments The concept of a Shuttle supporting the assembly of a space station was not an entirely new idea when Space Station Freedom was authorized in 1984. Such concepts had been evaluated during the late 1960s, as the United States and the Soviet Union competed in the race to the Moon. By the early 1970s, the two nations were on more friendly terms and keen to participate in a joint project as Apollo was being phased out and a series of Salyut space stations were being introduced. The American proposal for an Apollo to dock with a Salyut was rejected, as was a proposal to have a Soyuz dock with Skylab. So Apollo docked with Soyuz in the summer of 1975. That program was so successful that talks began almost immediately to assess the pros- pects for a Shuttle-Salyut docking in the early 1980s. In parallel, NASA devised plans for the Shuttle to reactivate Skylab. Neither of these proposals bore fruit. By the early 1980s, the idea of using a Shuttle to assemble and resupply a large space station remained, and would become the lynchpin of the Space Station Freedom before plans for that, too, were revised. By the time of the collapse of the Soviet Union in 1991 the assembly of Mir had been underway for several years. But Russia, which inherited the station and the spacecraft which serviced it, was hard pressed to continue the requisite funding. Looking back two decades to the 1990s, the merger of the American Shuttle and the Russian space station programs seems so logical, since they complemented each other.