Understanding Astronaut Shoulder Injury
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Supportability for Beyond Low Earth Orbit Missions
Supportability for Beyond Low Earth Orbit Missions William Cirillo1 and Kandyce Goodliff2 NASA Langley Research Center, Hampton, VA, 23681 Gordon Aaseng3 NASA Ames Research Center, Moffett Field, CA, 94035 Chel Stromgren4 Binera, Inc., Silver Springs, MD, 20910 and Andrew Maxwell5 Georgia Institute of Technology, Hampton, VA 23666 Exploration beyond Low Earth Orbit (LEO) presents many unique challenges that will require changes from current Supportability approaches. Currently, the International Space Station (ISS) is supported and maintained through a series of preplanned resupply flights, on which spare parts, including some large, heavy Orbital Replacement Units (ORUs), are delivered to the ISS. The Space Shuttle system provided for a robust capability to return failed components to Earth for detailed examination and potential repair. Additionally, as components fail and spares are not already on-orbit, there is flexibility in the transportation system to deliver those required replacement parts to ISS on a near term basis. A similar concept of operation will not be feasible for beyond LEO exploration. The mass and volume constraints of the transportation system and long envisioned mission durations could make it difficult to manifest necessary spares. The supply of on-demand spare parts for missions beyond LEO will be very limited or even non-existent. In addition, the remote nature of the mission, the design of the spacecraft, and the limitations on crew capabilities will all make it more difficult to maintain the spacecraft. Alternate concepts of operation must be explored in which required spare parts, materials, and tools are made available to make repairs; the locations of the failures are accessible; and the information needed to conduct repairs is available to the crew. -
Science in Nasa's Vision for Space Exploration
SCIENCE IN NASA’S VISION FOR SPACE EXPLORATION SCIENCE IN NASA’S VISION FOR SPACE EXPLORATION Committee on the Scientific Context for Space Exploration Space Studies Board Division on Engineering and Physical Sciences THE NATIONAL ACADEMIES PRESS Washington, D.C. www.nap.edu THE NATIONAL ACADEMIES PRESS 500 Fifth Street, N.W. Washington, DC 20001 NOTICE: The project that is the subject of this report was approved by the Governing Board of the National Research Council, whose members are drawn from the councils of the National Academy of Sciences, the National Academy of Engineering, and the Institute of Medicine. The members of the committee responsible for the report were chosen for their special competences and with regard for appropriate balance. Support for this project was provided by Contract NASW 01001 between the National Academy of Sciences and the National Aeronautics and Space Administration. Any opinions, findings, conclusions, or recommendations expressed in this material are those of the authors and do not necessarily reflect the views of the sponsors. International Standard Book Number 0-309-09593-X (Book) International Standard Book Number 0-309-54880-2 (PDF) Copies of this report are available free of charge from Space Studies Board National Research Council The Keck Center of the National Academies 500 Fifth Street, N.W. Washington, DC 20001 Additional copies of this report are available from the National Academies Press, 500 Fifth Street, N.W., Lockbox 285, Washington, DC 20055; (800) 624-6242 or (202) 334-3313 (in the Washington metropolitan area); Internet, http://www.nap.edu. Copyright 2005 by the National Academy of Sciences. -
Constellation Space Suit System Acquisition Schedule Plan
National Aeronautics and Space Administration ConstellationConstellation SpaceSpace Suit Suit SystemSystem ContractContract AwardAward AnnouncementAnnouncement DougDoug CookeCooke DeputyDeputy AssociateAssociate AdministratorAdministrator NASANASA ExplorationExploration SystemsSystems MissionMission DirectorateDirectorate JuneJune 12,12, 20082008 www.nasa.gov ConstellationConstellation SystemsSystems Division Extravehicular Activity – “EVA” • The space-suited astronaut is the ultimate symbol of human exploration • The spacesuit is essentially a self- contained, one-person spacecraft • It protects the crew from and enables them to work in the hostile environments of deep space and the lunar surface • It is the “last line of defense” for astronauts when they leave the relative safety of the crew exploration vehicle, lunar lander, or habitat 2 2 The Challenge for Exploration • Current spacesuits are not suitable for Exploration – Apollo Extravehicular Mobility Unit – Advanced Crew Escape Suit – Space Shuttle/International Space Station Extravehicular Mobility Unit • A new pressurized suit system will be required to support long-term Exploration requirements – Meets all capability requirements – Improves reliability – Improves logistics and maintenance – Reduces life cycle costs 3 3 The EVA System Design Approach Launch and Entry • A single spacesuit system with two configurations which share many components In-space Contingency • Common, evolvable infrastructure • Minimum set of hardware to meet all mission phase requirements • Modular, -
Testing of the Z-2 Space Suit at the Neutral Buoyancy Laboratory
47th International Conference on Environmental Systems ICES-2017-250 16-20 July 2017, Charleston, South Carolina Testing of the Z-2 Space Suit at the Neutral Buoyancy Laboratory Ian M. Meginnis,1 Richard A. Rhodes,2 Kristine N. Larson,3 and Amy J. Ross4 NASA Johnson Space Center, Houston, TX, 77058 The Z-2 space suit is the product of the last fifty years of NASA’s space suit research and testing experience. The Z-2 suit was originally developed as an exploration space suit for use on a planetary surface, such as the moon or Mars. However, Z-2 could also be used in microgravity at the International Space Station (ISS) to supplement or replace the existing extravehicular mobility unit (EMU). To evaluate the microgravity performance of Z-2 for compatibility at the ISS, the suit was tested in NASA’s Neutral Buoyancy Laboratory (NBL), which is the primary simulated microgravity testing environment for space suits. Seven test subjects, including five astronauts, performed various tasks that are representative of the tasks performed at the ISS. Test subjects performed tasks in the Z-2 suit and the EMU so that relative comparisons could be drawn between the two suits. Two configurations of the Z-2 space suit were evaluated during this test series: the EMU lower torso assembly (ELTA) configuration and the Z-2 lower torso assembly (ZLTA) configuration. The ELTA configuration, which was the primary test configuration, is comprised of the Z-2 upper torso and the EMU lower torso. The ZLTA configuration is comprised of the Z-2 upper torso and the Z-2 lower torso, which contains additional mobility elements. -
The EVA Spacesuit
POLITECNICO DI TORINO Repository ISTITUZIONALE Glove Exoskeleton for Extra-Vehicular Activities: Analysis of Requirements and Prototype Design Original Glove Exoskeleton for Extra-Vehicular Activities: Analysis of Requirements and Prototype Design / Favetto, Alain. - (2014). Availability: This version is available at: 11583/2546950 since: Publisher: Politecnico di Torino Published DOI:10.6092/polito/porto/2546950 Terms of use: openAccess This article is made available under terms and conditions as specified in the corresponding bibliographic description in the repository Publisher copyright (Article begins on next page) 04 August 2020 POLITECNICO DI TORINO DOCTORATE SCHOOL Ph. D. In Informatics and Systems – XXV cycle Doctor of Philosophy Thesis Glove Exoskeleton for Extra-Vehicular Activities Analysis of Requirements and Prototype Design (Part One) Favetto Alain Advisor: Coordinator: Prof. Giuseppe Carlo Calafiore Prof. Pietro Laface kp This page is intentionally left blank Dedicato a mio Padre... Al tuo modo ruvido di trasmettere le emozioni. Al tuo senso del dovere ed al tuo altruismo. Ai tuoi modi di fare che da piccolo non capivo e oggi sono parte del mio essere. A tutti i pensieri e le parole che vorrei averti detto e che sono rimasti solo nella mia testa. A te che mi hai sempre trattato come un adulto. A te che te ne sei andato prima che adulto lo potessi diventare davvero. opokp This page is intentionally left blank Index INDEX Index .................................................................................................................................................5 -
Balloon Astronaut San Jose, CA 95113 1-408-294-8324 Design Challenge Learning Thetech.Org
201 S. Market St. Balloon Astronaut San Jose, CA 95113 1-408-294-8324 Design Challenge Learning thetech.org Students investigate properties of materials and colliding objects by designing spacesuits for balloon astronauts. The objective is to design spacesuits that can withstand the hazards of high velocity impacts from space debris and meteoroids. As students iterate through this design challenge, they gain firsthand experience in the design process. Balloon Astronaut1 Grades 2-8 Estimated time: 45 minutes Student Outcomes: 1. Students will be able to design and build a protective device to keep their balloon astronaut from popping when impaled by a falling nail. 2. Students will be able to explain design considerations based on material characteristics, and concepts of energy, velocity, and the physics of colliding objects. 3. Students will be able to utilize the three step design process to meet an engineering challenge. Next Generation Science Standards Grade 2-5: Engineering Design K-2-ETS1-1, K-2-ETS1-2, K-2-ETS1-3, 3-5-ETS1-1, 3-5-ETS1-2, 3-5-ETS1-3 Grade 2: Physical Science 2-PS1-1, 2-PS1-2 Grade 3: Physical Science 3-PS2-1 Grade 4: Physical Science 4-PS3-1, 4-PS3-3, 4-PS3-4 Grade 5: Physical Science 5-PS2-1 Grade 6-8: Engineering Design MS-ETS1-1, MS-ETS1-2, MS-ETS1-3, MS-ETS1-4; Physical Science MS-PS2-1, MS-PS2-2, MS-PS3-2, MS-PS3-5 Common Core Language Arts-Speaking and Listening Grade 2: SL.2.1a-c, SL.2.3, SL.2.4a Grade 3: SL.3.1b-d, SL.3.3, SL.3.4a Grade 4: SL.4.1b-d, SL.4.4a Grade 5: SL.5.1b-d, SL.5.4 Grade 6: SL.6.1b-d Grade 7: SL.7.1b-d Grade 8: SL.8.1b-d California Science Content Grade 2: Physical Science 1.a-c; Investigation and Experimentation 4.a, 4.c-d Grade 3: Investigation and Experimentation 5.a-b, d Grade 4: Investigation and Experimentation 6.a, 6.c-d Grade 5: Investigation and Experimentation 6.a-c, 6.h Grade 6: Investigation and Experimentation 7.a-b, 7.d-e Grade 7: Investigation and Experimentation 7.a, 7.c-e Grade 8: Physical Science 1.a-e, 2.a-g; Investigation and Experimentation 9.b-c 1 Developed from a program designed by NASA. -
Repair Station Capabilities List
Approved by: Astronautics Corporation of America J. Simet, Repair Station Supervisor Approved by: TITLE: Astronautics Corp. of America Repair Station Capabilities List QAP 2003/2 REV. H J. Williams, Repair Station Accountable Manager CODE IDENT NO 10138 Page 1 of 35 Astronautics’ Capabilities List QAP 2003/2 Revision H QAP 2003/2 Astronautics Corporation of America REV SYM DESCRIPTION OF CHANGE DATE APPROVED A Initial Release. 3/25/2003 PFM B Updated to reflect FAA comments regarding when revisions will 1/16/2004 JT, DY, JGW be submitted. C Updated to change the preliminary XQAR449-P-L Repair 6/25/2004 JT, EF, JGW Station Number to XQAR449L. Added the 197800-1 & -3 DU, the 198200-1 & -3 EU, the 198000-( ) EFI and its 198040-( ) Control Panel, and the 260500-( ) EFI. App Added the PMA’d 197800-1 and -3 Display Unit, the 198200-1 6/25/2004 JGW A and -3 Electronics Unit, and the TSOA’d 198000-( ) EFI and its 198040-( ) Control Panel, and the 260500-( ) EFI. The self- evaluation for these items was performed under paragraph 5.5 (d) of this document. These FAA approvals were the basis for the additions. D Updated to separate Appendix A from the text (removed the date 11/30/2004 JT, EF, JGW on the cover sheet for the Appendix). The FAA will be sent a copy of the Appendix within ten days of the date on the Appendix whenever items are added or removed. The appendix will be controlled by date. A copy of the QAP cover sheet and text are controlled by revision letter, and a copy of that will be submitted to the FAA within ten days of the date that the new revision letter version of the text is released. -
Sg423finalreport.Pdf
Notice: The cosmic study or position paper that is the subject of this report was approved by the Board of Trustees of the International Academy of Astronautics (IAA). Any opinions, findings, conclusions, or recommendations expressed in this report are those of the authors and do not necessarily reflect the views of the sponsoring or funding organizations. For more information about the International Academy of Astronautics, visit the IAA home page at www.iaaweb.org. Copyright 2019 by the International Academy of Astronautics. All rights reserved. The International Academy of Astronautics (IAA), an independent nongovernmental organization recognized by the United Nations, was founded in 1960. The purposes of the IAA are to foster the development of astronautics for peaceful purposes, to recognize individuals who have distinguished themselves in areas related to astronautics, and to provide a program through which the membership can contribute to international endeavours and cooperation in the advancement of aerospace activities. © International Academy of Astronautics (IAA) May 2019. This publication is protected by copyright. The information it contains cannot be reproduced without written authorization. Title: A Handbook for Post-Mission Disposal of Satellites Less Than 100 kg Editors: Darren McKnight and Rei Kawashima International Academy of Astronautics 6 rue Galilée, Po Box 1268-16, 75766 Paris Cedex 16, France www.iaaweb.org ISBN/EAN IAA : 978-2-917761-68-7 Cover Illustration: credit A Handbook for Post-Mission Disposal of Satellites -
Constellation Space Suit System (CSSS) Title
The Future of U.S. Space Suits Presented by Carl Walz 9-22-2015 1 U.S. Space Suits – The Past 2 U.S. Space Suits – The Present 3 Future Human Exploration 4 New Space Suit Development Defining Questions • What Is The Destination And The Destination Environment • What Will Be The Host Spacecraft – What Is The Life Support Interface – What Is The Mechanical Interface • What Are The Mobility Requirements – Walking, Riding, or Both • What Size Suits Are Required – Suit Should Support A Larger Anthropometric Range • What Is The Logistical Plan – Suit Must Be Logistically Supportable For Long Periods of Time • What Is The Maintenance Plan – Suit Must Be Field Maintainable 5 NASA EVA Technology Development NASA Performed Yearly Test Campaigns In The Western U.S. To Develop Requirements For Planetary Surface EVAs EVA Pressure Garments At Field Testing, Flagstaff AZ 2006 6 NASA EVA Technology Development • Mark 3 Planetary Garment Designed For Surface EVAs – Hard Upper Torso And Hard Brief – Rear Entry – Walking Boots – Tested During Desert Rats Planetary Exploration Activities 7 NASA EVA Technology Development . ILC Dover I-Suit Pressure Garment – Soft Upper Torso And Soft Brief – Waist Or Rear Entry – Soft Lower Torso And Walking Boots – Tested At ILC And During Desert Rats Planetary Exploration Activities – Excellent Surface Mobility 8 NASA EVA Technology Development • The Z-1Pressure Garment Was Developed By NASA Under The Advanced Exploration Systems Program • Z-1 Suit Represents A Follow-On To The Mark 3 – Rear Entry – Hard Upper Torso And -
Complex Garment Systems to Survive in Outer Space
Volume 7, Issue 2, Fall 2011 Complex Garment Systems to Survive in Outer Space Debi Prasad Gon, Assistant Professor, Textile Technology, Panipat Institute of Engineering & Technology, Pattikalyana, Samalkha, Panipat, Haryana, INDIA [email protected] Palash Paul, Assistant Professor, Textile Technology, Panipat Institute of Engineering & Technology, Pattikalyana, Samalkha, Panipat, Haryana, INDIA ABSTRACT The success of astronauts in performing Extra-Vehicular Activity (EVA) is highly dependent on the performance of the spacesuit they are wearing. Since the beginning of the Space Shuttle Program, one basic suit design has been evolving. The Space Shuttle Extravehicular Mobility Unit (EMU) is a waist entry suit consisting of a hard upper torso (HUT) and soft fabric mobility joints. The EMU was designed specifically for zero gravity operations. With a new emphasis on planetary exploration, a new EVA spacesuit design is required. Now the research scientists are working hard and striving for the new, lightweight and modular designs. Thus they have reached to the Red surface of Mars. And sooner or later the astronauts will reach the other planets too. This paper is a review of various types of spacesuits and the different fabrics required for the manufacturing of the same. The detailed construction of EMU and space suit for Mars is discussed here, along with certain concepts of Biosuit- Mechanical Counter pressure Suit. Keywords: Extra-Vehicular Activity (EVA), spacesuits, Biosuit-Mechanical Counter pressure Suit Tissues (skin, heart, -
U.S. Spacesuit Knowledge Capture Accomplishments in Fiscal Year 2016
47th International Conference on Environmental Systems ICES-2017-47 16-20 July 2017, Charleston, SC U.S. Spacesuit Knowledge Capture Accomplishments in Fiscal Year 2016 Cinda Chullen 1 NASA Johnson Space Center, Houston, Texas, 77058 and Vladenka R. Oliva2 Jacobs Engineering Technology, Houston, Texas, 77058 As our nation focuses on its goal to visit Mars by the 2030s, the NASA U.S. Spacesuit Knowledge Capture (SKC) Program continues to serve the spacesuit community with a collection of spacesuit-related knowledge. Since its 2007 inception, the SKC Program has been collecting and archiving significant spacesuit-related knowledge and sharing it with various technical staff, along with invested and interested entities. The program has sponsored and recorded more than 80 events, and continues to build an electronic library of spacesuit knowledge. By the end of Fiscal Year (FY) 2016, 60 of these events were processed and uploaded to a publically accessible NASA Web site where viewers can broaden their knowledge about the spacesuit’s evolution, known capabilities, and lessons learned. Sharing this knowledge with entities beyond NASA, such as space partners and academia, provides a tremendous opportunity to expand and retain the knowledge of space. This valuable SKC Program now serves as an optimum means of archiving NASA’s spacesuit legacy from the Apollo era to the pursuit of Mars. This paper focuses on the FY 2016 SKC events, the release and accessibility of the approved events, and the program’s future plans. Nomenclature ARM = Asteroid -
Modeling Space Suit Mobility: Applications to Design and Operations
2001-01-2162 Modeling Space Suit Mobility: Applications to Design and Operations P. B. Schmidt and D. J. Newman Massachusetts Institute of Technology E. Hodgson Hamilton Sundstrand Space Systems International Copyright © 2001 Society of Automotive Engineers, Inc. ABSTRACT date repetitive tasks. Computer simulation also aids in future space suit design by allowing new space suit or Computer simulation of extravehicular activity (EVA) is component designs to be evaluated without the expense increasingly being used in planning and training for EVA. of constructing and certifying prototypes for human test- A space suit model is an important, but often overlooked, ing. While dynamic simulation is not currently used for component of an EVA simulation. Because of the inher- EVA planning, it has been used for post-flight analyses ent difficulties in collecting angle and torque data for [1, 2]. Other computer-based modeling and analysis space suit joints in realistic conditions, little data exists on techniques are used in pre-flight evaluations of EVA tasks the torques that a space suit’s wearer must provide in and worksites [3, 4]. order to move in the space suit. A joint angle and torque database was compiled on the Extravehicular Maneuver- An important shortcoming of current EVA models is that ing Unit (EMU), with a novel measurement technique that they lack an accurate representation of the torques that used both human test subjects and an instrumented are required to bend the joints of the space suit. The robot. Using data collected in the experiment, a hystere- shuttle EMU, like all pressurized space suits, restricts sis modeling technique was used to predict EMU joint joint motion to specific axes and ranges and has a ten- torques from joint angular positions.