Benefits of a Single-Person Spacecraft for Weightless Operations (Stop Walking and Start Flying)
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Design of a Human Settlement on Mars Using In-Situ Resources
46th International Conference on Environmental Systems ICES-2016-151 10-14 July 2016, Vienna, Austria Design of a Human Settlement on Mars Using In-Situ Resources Marlies Arnhof1 Vienna University of Technology, Vienna, 1040, Austria Mars provides plenty of raw materials needed to establish a lasting, self-sufficient human colony on its surface. Due to the planet's vast distance from Earth, it is neither possible nor economically reasonable to provide permanent, interplanetary supply. In-situ resource utilization (ISRU) will be necessary to keep the Earth launch burden and mission costs as low as possible, and to provide – apart from propellant and life support – a variety of construction material. However, to include outposts on other planets into the scope of human spaceflight also opens up new psychological and sociological challenges. Crews will live in extreme environments under isolated and confined conditions for much longer periods of time than ever before. Therefore, the design of a Mars habitat requires most careful consideration of physiological as well as psychosocial conditions of living in space. In this design for a Martian settlement, the author proposes that – following preliminary automated exploration – a basic surface base brought from Earth would be set up. Bags of unprocessed Martian regolith would be used to provide additional shielding for the habitat. Once the viability of the base and its production facilities are secured, the settlement would be expanded, using planetary resources. Martian concrete – processed regolith with a polymeric binder – would be used as main in-situ construction material. To provide optimum living and working conditions, the base would respond to the environment and the residents' number and needs, thereby evolving and growing continuously. -
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 -
Final Report of the International Space Station Independent Safety
I Contents Executive Summary........................................................................................ 1 Principal Observations ..................................................................................... 3 Principal Recommendations ............................................................................. 3 1. Introduction..................................................................................................... 5 Charter/Scope ................................................................................................... 5 Approach........................................................................................................... 5 Report Organization ......................................................................................... 5 2. The International Space Station Program.................................................... 7 International Space Station Characteristics..................................................... 8 3. International Space Station Crosscutting Management Functions............ 12 Robust On-Orbit Systems.................................................................................. 12 The Design ........................................................................................................ 12 Verification Requirements ................................................................................ 12 Physical (Fit) Verification ................................................................................ 13 Multi-element Integrated Test.......................................................................... -
Robotic Arm.Indd
Ages: 8-12 Topic: Engineering design and teamwork Standards: This activity is aligned to national standards in science, technology, health and mathematics. Mission X: Train Like an Astronaut Next Generation: 3-5-ETS1-2. Generate and compare multiple possible solutions to a problem based on how well each is likely A Robotic Arm to meet the criteria and constraints of the problem. 3-5-ETS1-3. Plan and carry out fair tests in which variables are controlled and failure points are considered to identify aspects of a model or prototype that can be EDUCATOR SECTION (PAGES 1-7) improved. STUDENT SECTION (PAGES 8-15) Background Why do we need robotic arms when working in space? As an example, try holding a book in your hands straight out in front of you and not moving them for one or two minutes. After a while, do your hands start to shake or move around? Imagine how hard it would be to hold your hands steady for many days in a row, or to lift something really heavy. Wouldn’t it be nice to have a really long arm that never gets tired? Well, to help out in space, scientists have designed and used robotic arms for years. On Earth, scientists have designed robotic arms for everything from moving heavy equipment to performing delicate surgery. Robotic arms are important machines that help people work on Earth as well as in space. Astronaut attached to a robotic arm on the ISS. Look at your arms once again. Your arms are covered in skin for protection. -
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. -
International Space Station Program Mobile Servicing System (MSS) To
SSP 42004 Revision E Mobile Servicing System (MSS) to User (Generic) Interface Control Document Part I International Space Station Program Revision E, May 22, 1997 Type 1 Approved by NASA National Aeronautics and Space Administration International Space Station Program Johnson Space Center Houston, Texas Contract No. NAS15–10000 SSP 42004, Part 1, Revision E May 22, 1997 REVISION AND HISTORY PAGE REV. DESCRIPTION PUB. DATE C Totally revised Space Station Freedom Document into an International Space Station Alpha Document 03–14–94 D Revision D reference PIRNs 42004–CS–0004A, 42004–NA–0002, 42004–NA–0003, TBD 42004–NA–0004, 42004–NA–0007D, 42004–NA–0008A, 42004–NA–0009C, 42004–NA–0010B, 42004–NA–0013A SSP 42004, Part 1, Revision E May 22, 1997 INTERNATIONAL SPACE STATION PROGRAM MOBILE SERVICING SYSTEM TO USER (GENERIC) INTERFACE CONTROL DOCUMENT MAY 22, 1997 CONCURRENCE PREPARED BY: PRINT NAME ORGN SIGNATURE DATE CHECKED BY: PRINT NAME ORGN SIGNATURE DATE SUPERVISED BY (BOEING): PRINT NAME ORGN SIGNATURE DATE SUPERVISED BY (NASA): PRINT NAME ORGN SIGNATURE DATE DQA: PRINT NAME ORGN SIGNATURE DATE i SSP 42004, Part 1, Revision E May 22, 1997 NASA/CSA INTERNATIONAL SPACE STATION PROGRAM MOBILE SERVICING SYSTEM (MSS) TO USER INTERFACE CONTROL DOCUMENT MAY 22, 1997 Print Name For NASA DATE Print Name For CSA DATE ii SSP 42004, Part 1, Revision E May 22, 1997 PREFACE SSP 42004, Mobile Servicing System (MSS) to User Interface Control Document (ICD) Part I shall be implemented on all new Program contractual and internal activities and shall be included in any existing contracts through contract changes. -
Suitport Feasibility - Development and Test of a Suitport and Space Suit for Human Pressurized Space Suit Donning Tests
Suitport Feasibility - Development and Test of a Suitport and Space Suit for Human Pressurized Space Suit Donning Tests Robert M. Boyle1, Kathryn Mitchell2, Charles Allton3, Hsing Ju4 Lyndon B. Johnson Space Center National Aeronautics and Space Administration Houston, Texas 77058 E-Mail: [email protected]; Phone: 281.483.5349 The suitport concept has been recently implemented as part of the small pressurized lunar rover (Currently the Space Exploration vehicle, or SEV) and the Multi-Mission Space Exploration Vehicle (MMSEV) concept demonstrator vehicle. Suitport replaces or augments the traditional airlock function of a spacecraft by providing a bulkhead opening, capture mechanism, and sealing system to allow ingress and egress of a space suit while the space suit remains outside of the pressurized volume of the spacecraft. This presents significant new opportunities to EVA exploration in both microgravity and surface environments. The suitport concept will enable three main improvements in EVA by providing reductions in: pre-EVA time from hours to less than thirty minutes; airlock consumables; contamination returned to the cabin with the EVA crewmember. To date, the first generation suitport has been tested with mockup suits on the rover cabins and pressurized on a bench top engineering unit. The work on the rover cabin has helped define the operational concepts and timelines, and has demonstrated the potential of suitport to save significant amounts of crew time before and after EVAs. The work with the engineering unit has successfully demonstrated the pressurizable seal concept including the ability to seal after the introduction and removal of contamination to the sealing surfaces. -
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. -
Interviews with the Apollo Lunar Surface Astronauts in Support of Planning for EVA Systems Design
NASA Technical Memorandum 108846 Interviews with the Apollo Lunar Surface Astronauts in Support of Planning for EVA Systems Design Mary M. Connors, Ames Research Center, Moffett Field, California Dean B. Eppler, SAIC, Houston, Texas Daniel G. Morrow, Decision Systems, Los Altos, California September 1994 NASA National Aeronautics and Space Administration Ames Research Center Moffett Field, California 94035-1000 Interviews with the Apollo Lunar Surface Astronauts in Support of Planning for EVA Systems Design MARY M. CONNORS, DEAN B. EPPLER,* AND DANIEL G. MORROW** Ames Research Center Summary was to explicate any other insights that could help further the planning process. Focused interviews were conducted with the Apollo astronauts who landed on the Moon. The purpose of The intended primary audience for this study is mission these interviews was to help define extravehicular activity planners and scientists and engineers responsible for (EVA) system requirements for future lunar and planetary EVA system design. However, we anticipate that various missions. Information from the interviews was examined aspects of the report may also be of interest to a wider with particular attention to identifying areas of consensus, readership and it is written to be accessible to anyone since some commonality of experience is necessary to aid with a general interest in EVA. the design of advanced systems. Results are presented This study followed a request made by the Office of under the following categories: mission approach; Exploration, NASA Headquarters, to the New Initiatives mission structure; suits; portable life support systems; Office at Johnson Space Center (JSC). The study team dust control; gloves; automation; information, displays, was headed by Robert Callaway of the New Initiative and controls; rovers and remotes; tools; operations; Office and included members of the Crew and Thermal training; and general comments. -
Extra-Vehicular Activity (EVA) and Mission Support Center (MSC)
Planetary Science Vision 2050 Workshop 2017 (LPI Contrib. No. 1989) 8201.pdf EXTRAVEHICULAR ACTIVITY (EVA) AND MISSION SUPPORT CENTER (MSC) DESIGN ELEMENTS FOR FUTURE HUMAN SCIENTIFIC EXPLORATION OF OUR SOLAR SYSTEM. M. J. Miller1, A. F. J. Abercromby2, S. Chappell2, K. Beaton2, S. Kobs Nawotniak3, A. L. Brady4, W. B. Garry5 and D. S. S. Lim6,7. 1Department of Aerospace Engineering, 270 Ferst Dr, Georgia Institute of Technology, Atlanta, GA 30313, [email protected]; 2NASA Johnson Space Center, 2101 NASA Parkway, Houston, TX 77058; 3Department of Geosciences, Idaho State University, 921 S. 8th Ave, M-S 8072, Pocatello, ID 83209; 4McMaster University, 1280 Main Street West, Hamilton, Ontario, Canada; 5NASA Goddard Space Flight Center, 8800 Green- belt Road, Greenbelt, MD, 20771; 6Bay Area Environmental Research Institute, 625 2nd St Ste. 209, Petaluma, CA 94952; 7NASA Ames Research Center, Moffett Field, CA 94035, [email protected] Introduction: NASA’s Journey to Mars outlines a ration involves peering into the unknown and reacting vision that includes sending humans to an asteroid by to the observed. The quest for scientific discovery is an 2025 and to Mars in the 2030s. While it is expected iterative and ceaseless process, as answers to research that most of the design elements for prospective capa- questions reveal more refined and sometimes unex- bilities and operational concepts will focus on issues pected research questions. In stark contrast, current concerning astronaut safety and planetary protection, EVA execution is highly scripted, with procedures we also envision mission architectures that are strongly arranged as a prioritized set of tasks, configured to driven by scientific requirements that fully leverage the maximize the likelihood of accomplishing the a priori presence of human assets in deep space.