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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 -
SPACE SUIT DEVELOPMENT STATUS by Richard S
NASA TECHNICAL NOTE NASA TN D-3291 -_ -_ c-- * a/ A KI R -1- i SPACE SUIT DEVELOPMENT STATUS by Richard S. Johnston, James V. Correale, and Matthew I. Radnofsky Manned Spacecraft Center Hozcston, Texas N AT10 N A 1 AERO N AUT1CS AND SPACE ADMINISTRATION WASHINGTON, D. C. FEBRUARY 1966 n TECH LIBRARY KAFB, NM , Illllll 11111 Illlll I llllllllll Ill1111 i 00797BL NASA 'I"D-3291 SPACE SUIT DEVELOPMENT STATUS By Richard S. Johnston, James V. Correale, and Matthew I. Radnofsky Manned Spacecraft Center Houston, Texas NATIONAL AERONAUTICS AND SPACE ADMINISTRATION For sale by the Clearinghouse for Federal Scientific and Technical Information Springfield, Virginia 22151 - Price $1.00 ABSTRACT Space suit development, starting with the Mercury program, has progressed to its present sta tus as a result of the changing goals of each manned spacecraft mission. The first space suits were de signed primarily for protection of flight crews against the possibility of cabin pressure failure. Longer flights and extravehicular activities required design philosophies to change drastically, particularly in the areas of comfort, mobility, reliability, and life- sustaining systems. Future mission goals will re quire new design objectives and requirements. ii SPACE SUIT DEVELOPMENT STATUS By Richard S. Johnston, James V. Correale, and Matthew I. Radnofsky Manned Spacecraft Center SUMMARY Space suits for the Mercury missions were designed primarily for pro tection of flight crews against the possibility of cabin pressure failure. How ever, goals of the Gemini program, particularly extravehicular activities, caused space suit design philosophies to change drastically. The suit had-to sustain life. A basic design was selected to satisfy all mission requirements. -
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, -
Physiology of Decompressive Stress
CHAPTER 3 Physiology of Decompressive Stress Jan Stepanek and James T. Webb ... upon the withdrawing of air ...the little bubbles generated upon the absence of air in the blood juices, and soft parts of the body, may by their vast numbers, and their conspiring distension, variously streighten in some places and stretch in others, the vessels, especially the smaller ones, that convey the blood and nourishment: and so by choaking up some passages, ... disturb or hinder the circulation of the blouod? Not to mention the pains that such distensions may cause in some nerves and membranous parts.. —Sir Robert Boyle, 1670, Philosophical transactions Since Robert Boyle made his astute observations in the Chapter 2, for details on the operational space environment 17th century, humans have ventured into the highest levels and the potential problems with decompressive stress see of the atmosphere and beyond and have encountered Chapter 10, and for diving related problems the reader problems that have their basis in the physics that govern this is encouraged to consult diving and hyperbaric medicine environment, in particular the gas laws. The main problems monographs. that humans face when going at altitude are changes in the gas volume within body cavities (Boyle’s law) with changes in ambient pressure, as well as clinical phenomena THE ATMOSPHERE secondary to formation of bubbles in body tissues (Henry’s law) secondary to significant decreases in ambient pressure. Introduction In the operational aerospace setting, these circumstances are Variations in Earthbound environmental conditions place of concern in high-altitude flight (nonpressurized aircraft limits and requirements on our activities. -
AIAA-95-1 062 the Suitport's Progress M. Cohen NASA Ames Research
NASA-TM-111836 /t/ .' I I AIAA-95-1 062 The Suitport's Progress M. Cohen NASA Ames Research Center Moffett Field, CA Life Sciences and Space Medicine Conference April 3-5, 1995 / Houston, TX For permission to copy or republish, contact the American Institute of Aeronautics and Astronautics 370 L'Enfant Promenade, SOW., Washington, D.C. 20024 AIAA-95-106; THE SUITPORT'S PROGRESS Marc M. Cohen* NASA-Ames Research Center Moffett Field, California Abstract Origins of the Suitport NASA-Ames Research Center developed The Suitport Extravehicular Access Facility the Suitport as an advanced space suit originated during the early phase of the airlock to support a Space Station suit, Space Station Advanced Development based on the AX-5 hard suit. Several third Program. It grew from a recognition that the parties proposed their own variations the construction and operation of Space Station Suitport on the moon and Mars. The Freedom (SSF) would require several Suitport recently found its first practical use thousand hours of EVA time (This finding as a terrestrial application in the NASA- has not changed much for the new design Ames Hazmat vehicle for the clean-up of for "Space Station Alpha." To make the best hazardous and toxic materials. In the Hazmat use of SSF crew time, it will become application, the Suitport offers substantial necessary to make the entire space suit improvements over conventional hazard donning and doffing, and airlock suits, by eliminating the necessicty to egress/ingress as safe, rapid, and efficient decontaminate before doffing the suit. as possible. Definitions The Space Shuttle EMU suit and airlock AX-5 Ames Experimental Suit 5 systems pose several potential CCPS Command/Control Pressure Suit disadvantages for frequent and routine EMU Extra-Vehicular Mobility Unit Space Station operations. -
Eva-Exp-0031 Baseline
EVA-EXP-0031 BASELINE National Aeronautics and EFFECTIVE DATE: 04/18/2018 Space Administration EVA OFFICE EXTRAVEHICULAR ACTIVITY (EVA) AIRLOCKS AND ALTERNATIVE INGRESS/EGRESS METHODS DOCUMENT The electronic version is the official approved document. ECCN Notice: This document does not contain export controlled technical data. Revision: Baseline Document No: EVA-EXP-0031 Release Date: 04/18/2018 Page: 2 of 143 Title: EVA Airlocks and Alternative Ingress Egress Methods Document REVISION AND HISTORY PAGE Revision Change Description Release No. No. Date EVA-EXP-0031 Baseline Baseline per CR# EVA-CR-00031 04/18/2018 Document dated 03/07/2018 submitted and approved through DAA process/DAA # TN54054 approved April 9, 2018 EVA-REF-001 DAA Pre Baseline 03/12/2015 33134 Draft EVA-RD-002 05/14/2015 SAA 12/15/2015 DRAFT The electronic version is the official approved document. ECCN Notice: This document does not contain export controlled technical data. Revision: Baseline Document No: EVA-EXP-0031 Release Date: 04/18/2018 Page: 3 of 143 Title: EVA Airlocks and Alternative Ingress Egress Methods Document Executive Summary This document captures the currently perceived vehicle and EVA trades with high level definition of the capabilities and interfaces associated with performing an Extravehicular Activity (EVA) using an exploration EVA system and ingress/egress methods during future missions. Human spaceflight missions to Cislunar space, Mars transit, the moons of Mars (Phobos and Deimos), the Lunar surface, and the surface of Mars will include both microgravity and partial-gravity EVAs, and potential vehicles with which an exploration EVA system will need to interface. -
ILC Space Suits & Related Products
ILC Space Suits & Related Products 0000-712731 Rev. A REVISIONS LETTER DESCRIPTION DATE - Initial Release 10/26/07 A Update with review comments and inclusion of the Antarctic Habitat and 11/28/07 Shuttle Adjustable Protective Mitten Assembly (APMA). This report was written through the volunteer efforts of ILC employees, retirees and friends. Additionally, this report would not have been possible without the efforts of Ken Thomas at Hamilton Sundstrand who truly realizes the significance of preserving the history of US space suit development. The information has been compiled to the best of the participant’s abilities given the volunteer nature of this effort. Any errors are unintentional and will be corrected once identified and verified. If there are any questions regarding any detail of this report, please call (302) 335-3911 Ext. 248. The production of this report does not imply ILC Dover agrees with or is responsible for the contents therein. This report has been compiled from information in the public domain and poses no export licensing issues. William Ayrey Primary Author & Publisher 2 ILC Space Suits & Related Products 0000-712731 Rev. A Table Of Content Chapter 1 The Path Leading To Space -------------------------------------------------------------------------------- 6 The XMC-2-ILC X-15 Competition Prototype (1957) --------------------------------------------------------- 6 The SPD-117 Mercury Competition Prototype (1959) --------------------------------------------------------- 8 Chapter 2 The Journey To The Moon (1960-72) --------------------------------------------------------------- 9 ILC Developments & Prototype Suits Leading To The Apollo Contract (1960-62)----------------------- 10 SPD-143 Training Suits -------------------------------------------------------------------------------------------- 14 Glove Development For Apollo And The World (1962-Present) -------------------------------------------- 17 AX1H - The First New Design Of The Apollo Program ------------------------------------------------------ 19 AX2H Suits (Sept. -
ICES-2019-173, the Space Activity Suit
https://ntrs.nasa.gov/search.jsp?R=20190027194 2019-09-26T19:05:13+00:00Z 49th International Conference on Environmental Systems ICES-2019-173 7-11 July 2019, Boston, Massachusetts The “Space Activity Suit” – A Historical Perspective and A Primer On The Physiology of Mechanical Counter-Pressure Shane M. McFarland1, Amy J. Ross2 and Dr. Robert W. Sanders, M.D.3 NASA Johnson Space Center, Houston, TX 77058 Since the 1950s, mechanical counter-pressure [MCP] has been investigated as a possible alternative design concept to traditional extra-vehicular activity [EVA] space suits. While traditional gas-pressurized EVA suits provide physiological protection against the ambient vacuum by means of pressurized oxygen to at least 3.1 psia (160 mmHg), MCP provides protection by direct application of pressure on the skin by a fabric. In reviewing the concept, MCP offers distinct potential advantages to traditional EVA suits: lower mass, reduced consumables, increased mobility, increased comfort, less complexity, and improved failure modes. In the mid 1960s to early 1970s, Dr. Paul Webb of Webb Associates developed and tested such a suit under funding from NASA Langley Research Center. This “Space Activity Suit” [SAS] was improved many times while testing in the laboratory and an altitude chamber to as low as 0.3 psia (15 mmHg). This testing, and the reports by Webb documenting it, are often presented as evidence of the feasibility of MCP. In addition, the SAS reports contain a wealth of information regarding the physiological requirements to make MCP work at the time, which is still accurate today. This paper serves to document the Space Activity Suit effort and analyze it in today’s context. -
CENTER SERIES SPACE SUITS Inventory
SPACE SUITS Rev Date:5/26/2000 Section 094 CENTER SERIES SPACE SUITS This subseries contains materials related to the development of space suits for intravehicular and extravehicular activity. As may be expected, the earliest space suits for the Mercury program descended from military pressure suits, in particular the Goodrich Navy Mark IV full pressure suit. The suit functioned primarily as protection against a sudden change in cabin pressure. It had no moveable bearings at the neck and wrist as did subsequent suits. The Gemini suit, too, is a version of a military suit developed by the David Clark Company for the USAF. Two versions, the G3C and G4C suits, were developed for intravehicular and extravehicular activity respectively. An additional suit, the G5C was developed for long duration flights. Since Gemini astronauts performed activities outside of the spacecraft, their space suits required thermal and micrometeoroid protection. Long term comfort also became necessary as mission duration increased. Naturally, the unique requirements of a lunar landing dictated changes in the space suits worn during lunar exploration excursions. The Apollo EMU (extravehicular mobility unit) required unlimited mobility, thermal, micrometeoroid and visual protection systems, a four hour lunar surface time, and compatibility with the CSM under pressurized and unpressurized conditions. The EMU included a water cooled under garment and a backpack (PLSS) housing all life support, communications and biomedical telemetry systems. Hamilton Standard had overall responsibility for the Apollo suit and portable life support system. International Latex Corporation held the production contract. Life support systems for the AAP / Skylab program were developed and built by the Garrett Corporation. -
Advanced Two-System Space Suit University of California, Berkeley
Advanced Two-System Space Suit University of California, Berkeley Team Members: Camron Gorguinpour Raven LeClair Daniel Carval Matt Estes Andy Hsieh Kirsten Howe Carlos Rodriguez Mujtaba Saffuden Sam Saylor Yung-Ruey Yen Faculty Advisors: Prof. Tom Budinger, chair Department of Bioengineering. Dr. Larry Kuznetz, former NASA scientist. Abstract We present the results of our research into the development of an advanced space suit design, based on the concept of separating the head and torso pressurization systems. Summary Current Extravehicular Mobility Units (EMU’s) must be improved for use in long- duration extravehicular activities (EVA's), as they are at risk of exposing the astronaut to explosive decompression, relatively inefficient in resource consumption, cumbersome, and expensive to maintain due to their complexity. To attack some of these issues, it is the aim of this project to design and develop a two-component space suit—a head bubble and a pressurized body suit—connected to each other through a neck-dam system. The separation of the head from the body will allow the astronaut more time to reach safety in the case of decompression and minimize O2 loss by allowing for independent pressurization of the body and eliminating loss through the soft joints. Moreover, concurrent research on pressurization methods for the body-- with emphasis on mechanical counter-pressure and the use of dense polyurethane membranes—will pave the way toward a more practical, mobile, and inexpensive unit. For the success of the two-chamber space suit (TCSS) idea, design and functionality of the neck-dam system is vital. As outlined below, the neck-dam system and our ideas for body-suit pressurization show a strong potential for space-flight applicability, thereby, allowing engineers to modify the current EMU to provide maximum resource efficiency, while maximizing safety, reliability, and mobility. -
Find Ebook » Spacesuits
N7WVTXYEZ2NE \\ Kindle \\ Spacesuits Spacesuits Filesize: 3.98 MB Reviews This book might be well worth a study, and much better than other. Indeed, it can be perform, continue to an amazing and interesting literature. I realized this publication from my i and dad suggested this book to find out. (Dejuan Rippin) DISCLAIMER | DMCA JTDJHKOVURP7 > Book Spacesuits SPACESUITS Reference Series Books LLC Jan 2012, 2012. Taschenbuch. Book Condition: Neu. 248x189x10 mm. This item is printed on demand - Print on Demand Neuware - Source: Wikipedia. Pages: 37. Chapters: American spacesuits, Soviet and Russian spacesuits, Space suit components, Apollo/Skylab A7L, Sokol space suit, Space activity suit, Extravehicular Mobility Unit, Gemini space suit, Orlan space suit, Navy Mark IV, Advanced Crew Escape Suit, Constellation Space Suit, Suitport, Liquid Cooling and Ventilation Garment, Launch Entry Suit, Primary Life Support System, Carbon dioxide scrubber, Krechet-94, I-Suit, Feitian space suit, Mark III, Strizh, Thermal Micrometeoroid Garment, SK-1 spacesuit, Yastreb, Hard Upper Torso, Berkut spacesuit, Maximum Absorbency Garment, Shuttle Ejection Escape Suit. Excerpt: The A7L Apollo & Skylab spacesuit is the primary pressure suit worn by NASA astronauts for Project Apollo, the three manned Skylab flights, and the Apollo-Soyuz Test Project between 1968 and the termination of the Apollo program in 1975. The 'A7L' designation is used by NASA as the seventh Apollo spacesuit designed and built by ILC Dover. The A7L is a design evolution of ILC's A5L and A6L. The A5L was the initial design. The A6L introduced the integrated thermal and micrometeroid cover layer. Aer the AS-204 spacecra fire, the suit was upgraded to be fire-resistant and given the designation A7L. -
Space Suit Concepts and Vehicle Interfaces for the Constellation Program
Publications 7-9-2007 Space Suit Concepts and Vehicle Interfaces for the Constellation Program D. M. Klaus University of Colorado Boulder J. Metts University of Colorado Boulder R. Kobrick University of Colorado Boulder, [email protected] M. Mesloh University of Colorado Boulder T. Monk University of Colorado Boulder See next page for additional authors Follow this and additional works at: https://commons.erau.edu/publication Part of the Space Vehicles Commons Scholarly Commons Citation Klaus, D. M., Metts, J., Kobrick, R., Mesloh, M., Monk, T., & et al. (2007). Space Suit Concepts and Vehicle Interfaces for the Constellation Program. , (). https://doi.org/10.4271/2007-01-3088 This is a publication from SAE International. This Presentation without Video is brought to you for free and open access by Scholarly Commons. It has been accepted for inclusion in Publications by an authorized administrator of Scholarly Commons. For more information, please contact [email protected]. Authors D. M. Klaus, J. Metts, R. Kobrick, M. Mesloh, T. Monk, and et al. This presentation without video is available at Scholarly Commons: https://commons.erau.edu/publication/532 Downloaded from SAE International by Embry Riddle Aeronautical University, Wednesday, August 23, 2017 SAE TECHNICAL PAPER SERIES 2007-01-3088 Space Suit Concepts and Vehicle Interfaces for the Constellation Program D. M. Klaus, J. Metts, R. Kobrick, M. Mesloh, T. Monk, E. Gauthier, K. Eberhart, D. Baca, C. Wright, A. Gustafson, L. Oryshchyn and D. Massey University of Colorado at Boulder 37th International Conference on Environmental Systems (ICES) Chicago, Illinois July 9-12, 2007 400 Commonwealth Drive, Warrendale, PA 15096-0001 U.S.A.