Under Pressure: by Phillip Keane a Brief History of Pressure Suits Part 1
Total Page:16
File Type:pdf, Size:1020Kb
Load more
Recommended publications
-
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, -
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. -
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 -
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. -
Requirements and Sizing Investigation for Constellation Space Suit Portable Life Support System Trace Contaminant Control
Requirements and Sizing Investigation for Constellation Space Suit Portable Life Support System Trace Contaminant Control Heather L. Paul and Mallory A. Jennings NASA Johnson Space Center Glenn Waguespack Geocontrol Systems, Inc. Abstract The Trace Contaminant Control System (TCCS), located within the ventilation loop of the Constellation Space Suit Portable Life Support System (PLSS), is responsible for removing hazardous trace contaminants from the space suit ventilation flow. This paper summarizes the results of a trade study that evaluated if trace contaminant control could be accomplished without a TCCS, relying on suit leakage, ullage loss from the carbon dioxide and humidity control system, and other factors. Trace contaminant generation rates were revisited to verify that values reflect the latest designs for Constellation Space Suit System (CSSS) pressure garment materials and PLSS hardware. Additionally, TCCS sizing calculations were performed and a literature survey was conducted to review the latest developments in trace contaminant technologies. \ Introduction The Constellation program operational concepts documents ([1] and [2]) require the ability to perform suited Extravehicular Activities (EVAs) on the lunar surface for lunar sorties, cargo unloading operations, extended stay operations, and continuous presence operations. Each EVA can last up to 8 hours. No nominal EVAs are currently planned for non-lunar-surface operations using Constellation assets. The second configuration of the CSSS, known as “Configuration 2,” is being developed to provide a self-contained, pressurized, portable environment to accommodate the lunar EVA requirements. A crucial component of the Configuration 2 suit system is the PLSS, which provides oxygen (O2) for breathing and pressurization, removes metabolically-produced carbon dioxide (CO2), removes trace contaminants produced by material and crewmember off-gassing, and regulates the thermal environment of the crewmember. -
US Spacesuits
springer.com Kenneth S. Thomas, Harold J. McMann U. S. Spacesuits Series: Space Exploration Remains the most comprehensive text on U.S. spacesuits and their development available Contains many new insights and photographs on space suits used for different manned missions that were not in the first edition Explains the function, historical development, and use of spacesuits from a worldwide perspective Provides details on NASA's new Constellation Spacesuit System Spacesuits are far more than garments. They are a personalized spacecraft that allows direct contact and interaction with everything beyond our world, and a last refuge for survival in a disaster. Creating safe, reliable, and comfortable spacesuits is an ongoing challenge that has spanned over four decades. "U. S. Spacesuits, 2nd Edition" by Kenneth S. Thomas and Harold J. McMann details the technical evolution of U. S. spacesuits from their roots in high altitude 2nd ed. 2012, XXXV, 472 p. 284 illus., 124 aviation and vacuum tube development to present day, with an additional look into the future. illus. in color. This primary source of spacesuit information explains the functions, historical development, and use of spacesuits from a worldwide perspective. In this new edition, the authors update the Printed book story of U.S. spacesuit development and efforts, from the design challenges modern engineers Softcover face to the latest roles of spacesuits in space exploration. The book also provides a close up 44,99 € | £39.99 | $54.99 look at NASA's new Constellation Space Suit System as well as Apollo prototype configurations [1] 48,14 € (D) | 49,49 € (A) | CHF that have been discovered since 2005. -
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.